Patent Publication Number: US-2023155242-A1

Title: System and method for battery ventilation of an electric aircraft

Description:
FIELD OF THE INVENTION 
     The present invention generally relates to the field of battery ventilation. In particular, the present invention is directed to a system and method for battery ventilation of an electric aircraft. 
     BACKGROUND 
     Electric aircraft include batteries to operate. Batteries are prone to overheating during flight, charging, or other operations. Modern ventilation systems are inefficient at reducing temperatures of batteries and can be improved. 
     SUMMARY OF THE DISCLOSURE 
     In an aspect, a system for battery ventilation of an electric aircraft. A system includes an electric aircraft. An electric aircraft includes a plurality of battery cells. Each battery cell of the plurality of battery cells includes a heat-conducting battery tab. A system includes a sensor. A sensor is in electronic communication with a plurality of battery cells. A sensor is configured to measure battery cell data. A system includes a plurality of vents. Each vent of the plurality of vents is positioned by each battery tab of the plurality of battery cells. Each vent of a plurality of vents includes an actuator configured to selectively open and close the vent. A system includes a flight controller. A flight controller is configured to receive battery cell data from a sensor. A flight controller is configured to determine a vent arrangement as a function of battery cell data. A flight controller is configured to control at least an actuator corresponding to at least a vent of a plurality of vents as a function of a vent arrangement. 
     In another aspect, a method of battery ventilation for an electric aircraft. A method includes providing a plurality of vents to a plurality of battery cells of an electric aircraft. A method includes sensing via a sensor in electronic communication with a plurality of battery cells battery cell data. A method includes determining via a flight controller of an electric aircraft a vent arrangement. A method includes adjusting at least a vent of a plurality of vents as a function of a vent arrangement. 
     These and other aspects and features of non-limiting embodiments of the present invention will become apparent to those skilled in the art upon review of the following description of specific non-limiting embodiments of the invention in conjunction with the accompanying drawings. 
    
    
     
       BRIEF DESCRIPTION OF THE DRAWINGS 
       For the purpose of illustrating the invention, the drawings show aspects of one or more embodiments of the invention. However, it should be understood that the present invention is not limited to the precise arrangements and instrumentalities shown in the drawings, wherein: 
         FIG.  1    is an illustration of an exemplary embodiment of an electric aircraft;  FIG.  2    is a block diagram of an exemplary embodiment of a ventilation system;  FIG.  3    is an illustration of a vent arrangement;  FIG.  4    is a block diagram of a battery management system;  FIG.  5    is a block diagram of an exemplary embodiment of a flight controller;  FIG.  6    is a block diagram of an exemplary machine-learning process;  FIG.  7    is a flowchart of a method of battery ventilation for an electric aircraft; and  FIG.  8    is a block diagram of a computing system that can be used to implement any one or more of the methodologies disclosed herein and any one or more portions thereof. 
     
    
    
     The drawings are not necessarily to scale and may be illustrated by phantom lines, diagrammatic representations and fragmentary views. In certain instances, details that are not necessary for an understanding of the embodiments or that render other details difficult to perceive may have been omitted. 
     DETAILED DESCRIPTION 
     Described herein is a system for battery ventilation of an electric aircraft. A system may include an electric aircraft. An electric aircraft may include a plurality of battery cells. Each battery cell of the plurality of battery cells may include a heat-conducting battery tab. A system may include a sensor. A sensor may be in electronic communication with a plurality of battery cells. A sensor may be configured to measure battery cell data. A system may include a plurality of vents. Each vent of a plurality of vents may be positioned by each battery tab of a plurality of battery cells. Each vent of a plurality of vents may include an actuator configured to selectively open and close the vent. A system may include a flight controller. A flight controller may be configured to receive battery cell data from a sensor. A flight controller may be configured to determine a vent arrangement as a function of battery cell data. A flight controller may be configured to control at least an actuator corresponding to at least a vent of a plurality of vents as a function of a vent arrangement. 
     Described herein is a method of battery ventilation for an electric aircraft. A method may include providing a plurality of vents to a plurality of battery cells of an electric aircraft. A method may include sensing via a sensor in electronic communication with a plurality of battery cells battery cell data. A method may include determining via a flight controller of an electric aircraft a vent arrangement. A method may include adjusting at least a vent of a plurality of vents as a function of a vent arrangement. 
     Referring now to  FIG.  1   , an embodiment of an electric aircraft  100  is presented. Still referring to  FIG.  1   , electric aircraft  100  may include a vertical takeoff and landing aircraft (eVTOL). As used herein, a vertical take-off and landing (eVTOL) aircraft is one that can hover, take off, and land vertically. An eVTOL, as used herein, is an electrically powered aircraft typically using an energy source, of a plurality of energy sources to power the aircraft. In order to optimize the power and energy necessary to propel the aircraft, eVTOL may be capable of rotor-based cruising flight, rotor-based takeoff, rotor-based landing, fixed-wing cruising flight, airplane-style takeoff, airplane-style landing, and/or any combination thereof. Rotor-based flight, as described herein, is where the aircraft generated lift and propulsion by way of one or more powered rotors coupled with an engine, such as a “quad copter,” multi-rotor helicopter, or other vehicle that maintains its lift primarily using downward thrusting propulsors. Fixed-wing flight, as described herein, is where the aircraft is capable of flight using wings and/or foils that generate life caused by the aircraft&#39;s forward airspeed and the shape of the wings and/or foils, such as airplane-style flight. 
     With continued reference to  FIG.  1   , a number of aerodynamic forces may act upon the electric aircraft  100  during flight. Forces acting on an electric aircraft  100  during flight may include, without limitation, thrust, the forward force produced by the rotating element of the electric aircraft  100  and acts parallel to the longitudinal axis. Another force acting upon electric aircraft  100  may be, without limitation, drag, which may be defined as a rearward retarding force which is caused by disruption of airflow by any protruding surface of the electric aircraft  100  such as, without limitation, the wing, rotor, and fuselage. Drag may oppose thrust and acts rearward parallel to the relative wind. A further force acting upon electric aircraft  100  may include, without limitation, weight, which may include a combined load of the electric aircraft  100  itself, crew, baggage, and/or fuel. Weight may pull electric aircraft  100  downward due to the force of gravity. An additional force acting on electric aircraft  100  may include, without limitation, lift, which may act to oppose the downward force of weight and may be produced by the dynamic effect of air acting on the airfoil and/or downward thrust from the propulsor of the electric aircraft. Lift generated by the airfoil may depend on speed of airflow, density of air, total area of an airfoil and/or segment thereof, and/or an angle of attack between air and the airfoil. For example, and without limitation, electric aircraft  100  are designed to be as lightweight as possible. Reducing the weight of the aircraft and designing to reduce the number of components is essential to optimize the weight. To save energy, it may be useful to reduce weight of components of an electric aircraft  100 , including without limitation propulsors and/or propulsion assemblies. In an embodiment, the motor may eliminate need for many external structural features that otherwise might be needed to join one component to another component. The motor may also increase energy efficiency by enabling a lower physical propulsor profile, reducing drag and/or wind resistance. This may also increase durability by lessening the extent to which drag and/or wind resistance add to forces acting on electric aircraft  100  and/or propulsors. 
     Referring still to  FIG.  1   , electric aircraft  100  may include at least a vertical propulsor  104  and at least a forward propulsor  108 . A forward propulsor is a propulsor that propels the aircraft in a forward direction. Forward in this context is not an indication of the propulsor position on the aircraft. One or more forward propulsors may be mounted on the front, on the wings, at the rear, etc. A vertical propulsor is a propulsor that propels the aircraft in an upward direction; one of more vertical propulsors may be mounted on the front, on the wings, at the rear, and/or any suitable location. A propulsor, as used herein, is a component or device used to propel a craft by exerting force on a fluid medium, which may include a gaseous medium such as air or a liquid medium such as water. At least a vertical propulsor  104  is a propulsor that generates a substantially downward thrust, tending to propel an aircraft in a vertical direction providing thrust for maneuvers such as without limitation, vertical take-off, vertical landing, hovering, and/or rotor-based flight such as “quadcopter” or similar styles of flight. 
     With continued reference to  FIG.  1   , at least a forward propulsor  108  as used in this disclosure is a propulsor positioned for propelling an aircraft in a “forward” direction; at least a forward propulsor may include one or more propulsors mounted on the front, on the wings, at the rear, or a combination of any such positions. At least a forward propulsor may propel an aircraft forward for fixed-wing and/or “airplane”-style flight, takeoff, and/or landing, and/or may propel the aircraft forward or backward on the ground. At least a vertical propulsor  104  and at least a forward propulsor  108  includes a thrust element. At least a thrust element may include any device or component that converts the mechanical energy of a motor, for instance in the form of rotational motion of a shaft, into thrust in a fluid medium. At least a thrust element may include, without limitation, a device using moving or rotating foils, including without limitation one or more rotors, an airscrew or propeller, a set of airscrews or propellers such as contrarotating propellers, a moving or flapping wing, or the like. At least a thrust element may include without limitation a marine propeller or screw, an impeller, a turbine, a pump-jet, a paddle or paddle-based device, or the like. As another non-limiting example, at least a thrust element may include an eight-bladed pusher propeller, such as an eight-bladed propeller mounted behind the engine to ensure the drive shaft is in compression. Propulsors may include at least a motor mechanically coupled to the at least a first propulsor as a source of thrust. A motor may include without limitation, any electric motor, where an electric motor is a device that converts electrical energy into mechanical energy, for instance by causing a shaft to rotate. At least a motor may be driven by direct current (DC) electric power; for instance, at least a first motor may include a brushed DC at least a first motor, or the like. At least a first motor may be driven by electric power having varying or reversing voltage levels, such as alternating current (AC) power as produced by an alternating current generator and/or inverter, or otherwise varying power, such as produced by a switching power source. At least a first motor may include, without limitation, brushless DC electric motors, permanent magnet synchronous at least a first motor, switched reluctance motors, or induction motors. In addition to inverter and/or a switching power source, a circuit driving at least a first motor may include electronic speed controllers or other components for regulating motor speed, rotation direction, and/or dynamic braking. Persons skilled in the art, upon reviewing the entirety of this disclosure, will be aware of various devices that may be used as at least a thrust element. 
     With continued reference to  FIG.  1   , during flight, a number of forces may act upon the electric aircraft. Forces acting on an aircraft  100  during flight may include thrust, the forward force produced by the rotating element of the aircraft  100  and acts parallel to the longitudinal axis. Drag may be defined as a rearward retarding force which is caused by disruption of airflow by any protruding surface of the aircraft  100  such as, without limitation, the wing, rotor, and fuselage. Drag may oppose thrust and acts rearward parallel to the relative wind. Another force acting on aircraft  100  may include weight, which may include a combined load of the aircraft  100  itself, crew, baggage and fuel. Weight may pull aircraft  100  downward due to the force of gravity. An additional force acting on aircraft  100  may include lift, which may act to oppose the downward force of weight and may be produced by the dynamic effect of air acting on the airfoil and/or downward thrust from at least a propulsor. Lift generated by the airfoil may depends on speed of airflow, density of air, total area of an airfoil and/or segment thereof, and/or an angle of attack between air and the airfoil. 
     Referring now to  FIG.  2   , system  200  for battery ventilation is presented. System  200  may include electric aircraft  204 . Electric aircraft  204  may include, but is not limited to, an unmanned aerial vehicle (UAV), helicopter, drone, eVTOL, and the like. Electric aircraft  204  may be as described above with reference to  FIG.  1   . 
     Still referring to  FIG.  2   , electric aircraft  204  may include battery cells  208 . Battery cells  208  may each include a cell configured to include an electrochemical reaction that may produce electrical energy sufficient to power at least a portion of electric aircraft  204 . Battery cells  208  may include, but are not limited to, electrochemical cells, galvanic cells, electrolytic cells, fuel cells, flow cells, voltaic cells, or any combination thereof. In some embodiments, battery cells  208  may be electrically connected in series, in parallel, or a combination of series and parallel. Series connection, as used herein, comprises wiring a first terminal of a first cell to a second terminal of a second cell and further configured to comprise a single conductive path for electricity to flow while maintaining the same current (measured in Amperes) through any component in the circuit. Battery cells  208  may use the term ‘wired’, but one of ordinary skill in the art would appreciate that this term is synonymous with ‘electrically connected’, and that there are many ways to couple electrical elements like battery cells  208  together. As an example, battery cells  208  may be coupled via prefabricated terminals of a first polarity that mate with a second terminal with a second polarity. Parallel connection, as used herein, comprises wiring a first and second terminal of a first battery cell to a first and second terminal of a second battery cell and further configured to comprise more than one conductive path for electricity to flow while maintaining the same voltage (measured in Volts) across any component in the circuit. Battery cells  208  may be wired in a series-parallel circuit which combines characteristics of the constituent circuit types to this combination circuit. Battery cells  208  may be electrically connected in any arrangement which may confer onto the system the electrical advantages associated with that arrangement such as high-voltage applications, high-current applications, or the like. 
     Still referring to  FIG.  2   , as used herein, an electrochemical cell is a device capable of generating electrical energy from chemical reactions or using electrical energy to cause chemical reactions. Further, voltaic or galvanic cells are electrochemical cells that generate electric current from chemical reactions, while electrolytic cells generate chemical reactions via electrolysis. As used herein, the term ‘battery’ is used as a collection of battery cells connected in series or parallel to each other. In some embodiments, battery cells  208  may include pouch cells. As used in this disclosure, “pouch cell” is any battery cell or module that includes a pocket. In some cases, a pouch cell may include or be referred to as a prismatic pouch cell, for example when an overall shape of pouch is prismatic. In some cases, a pouch cell may include a pouch which is substantially flexible. Alternatively or additionally, in some cases, a pouch may be substantially rigid. In some cases, a pouch may include a polymer, such as without limitation polyethylene, acrylic, polyester, and the like. In some embodiments, a pouch may be coated with one or more coatings. For example, in some cases, a pouch may have an outer surface. In some embodiments, an outer surface may be coated with a metalizing coating, such as an aluminum or nickel containing coating. In some embodiments, a pouch coating may be configured to electrically ground and/or isolate pouch, increase pouch impermeability, increase pouches resistance to high temperatures, increases pouches thermal resistance (insulation), and the like. An electrolyte may be located in a pouch. In some embodiments, an electrolyte may include a liquid, a solid, a gel, a paste, and/or a polymer. In some embodiments, an electrolyte may include a lithium salt such as LiPF 6 . In some embodiments, a lithium salt may include lithium hexafluorophosphate, lithium tetrafluoroborate, lithium perchlorate, or other lithium salts. In some embodiments, a lithium salt may include an organic solvent. In some embodiments, an organic solvent may include ethylene carbonate, dimethyl carbonate, diethyl carbonate or other organic solvents. In some embodiments, an electrolyte may wet or contact one or both of a pair of conductive tabs of a battery cell. A “conductive tab” as used in this disclosure is any protruding component capable of carrying a current. In some embodiments, each battery cell of battery cells  208  may include a conductive tab that may extrude from a side of the battery cell. In some embodiments, a conductive tab may extrude from a bottom, side, rear, top, or front surface of a battery cell of battery cells  208 . In some embodiments, a conductive tab of each battery cell of battery cells  208  may be configured to conduct heat. 
     Still referring to  FIG.  2   , battery cells  208  may include without limitation a battery cell using nickel-based chemistries such as nickel cadmium or nickel metal hydride, a battery cell using lithium-ion battery chemistries such as a nickel cobalt aluminum (NCA), nickel manganese cobalt (NMC), lithium iron phosphate (LiFePO4), lithium cobalt oxide (LCO), lithium manganese oxide (LMO), a battery cell using lithium polymer technology, and/or metal-air batteries. Battery cells  208  may include lead-based batteries such as without limitation lead acid batteries and lead carbon batteries. Battery cells  208  may include lithium sulfur batteries, magnesium ion batteries, and/or sodium ion batteries. Battery cells  208  may include solid state batteries or supercapacitors or another suitable energy source. Persons skilled in the art, upon reviewing the entirety of this disclosure, will be aware of various devices of components that may be used as a battery cell. 
     Still referring to  FIG.  2   , electric aircraft  204  may include vents  212 . A “vent” as used in this disclosure is any device capable of directing an airflow. In some embodiments, vents  212  may include a metallic, polymer, or other component. In some embodiments, vents  212  may include a shape. A shape may include, but is not limited to, a rectangle, square, triangle, circle, hexagon, prism, or other shapes. In some embodiments, vents  212  may include a curved structure. In some embodiments, vents  212  may include a smooth surface. Vents  212  may include a uniform structure. In other embodiments, vents  212  may include openings such as holes, slits, or other openings. In some embodiments, vents  212  may include one or more apertures. An “aperture” as used in this disclosure is an opening configured to allow a medium to pass through. In some embodiments, an aperture may include, but is not limited to, a flap, a door, a hole, and the like. In some embodiments, an aperture of vents  212  may be moved as a function of actuator  230 . An “actuator” as used in this disclosure is a device that converts a signal into mechanical and/or electromechanical motion. In some embodiments, actuator  320  may include, but is not limited to, pneumatic, hydraulic, mechanical, and/or an electronic actuator. Actuator  320  may include an electronically actuated device such as, but not limited to, a servo, an electromotor, and the like. Computing device  220  may be command actuator  230  to control an aperture of one or more vents of vents  212 . Actuator  230  may be configured to increase and/or decrease a size of an aperture of vents  212 . In some embodiments, actuator  230  may be configured to direct a flow of air through an aperture of vents  212 . In some embodiments, actuator  230  may adjust an angle and/or orientation of an aperture of vents  212 . In a non-limiting example, actuator  230  may adjust an angle of a plurality of apertures of vents  212  which may direct a heated air away from battery cells  208 . In another non-limiting example, actuator  230  may reduce a diameter of an aperture of vents  212  which may prevent external elements from contacting battery cells  208 . In some embodiments, each vent of vents  212  may include an actuator  230 . In some embodiments, actuator  230  may adjust an aperture of each vent of vents  212  individually. In other embodiments, actuator  230  may adjust a plurality of apertures of vents  212 . Each vent of vents  212  may be paired to each battery cell of battery cells  208 . In some embodiments, vents  212  may be positioned underneath battery cells  208 . In some embodiments, vents  212  may be positioned above, behind, and/or at a side of battery cells  208 . In some embodiments, vents  212  may include an orientation. An “orientation” as used in this disclosure is any direction, rotation, and/or or angle of an object. In some embodiments, each vent of vents  212  may include a similar orientation. In other embodiments, each vent of vents  212  may have an orientation different from one another. In some embodiments, vents  212  may include a moveable component. A “moveable component” as used in this disclosure is any device capable of changing a position. In some embodiments, a moveable component may include, but is not limited to, a motor, actuator, and the like. A motor may include an electromechanical motor, servo motor, or other motors. An actuator include a hydraulic, pneumatic, electric, and/or other actuator. In some embodiments, each vent of vents  212  may include an individual movable component. An individual movable component may be configured to adjust a vent of vents  212  separately from other vents of vents  212 . 
     Still referring to  FIG.  2   , electric aircraft  204  may include sensor  216 . Sensor  216  may be coupled to battery cells  208 . In some embodiments, sensor  216  may be mechanically and/or electrically coupled to battery cells  208 . Sensor  216  may include a plurality of sensors in the form of individual sensors or a sensor suite working in tandem or individually. A sensor suite may include a plurality of independent sensors, as described herein, where any number of the described sensors may be used to detect any number of physical or electrical quantities associated with an aircraft power system or an electrical energy storage system. Independent sensors may include separate sensors measuring physical or electrical quantities that may be powered by and/or in communication with circuits independently, where each may signal sensor output to a control circuit such as a user graphical interface. In a non-limiting example, there may be four independent sensors housed in and/or on battery cells  208  measuring temperature, electrical characteristic such as voltage, amperage, resistance, or impedance, or any other parameters and/or quantities as described in this disclosure. In an embodiment, use of a plurality of independent sensors may result in redundancy configured to employ more than one sensor that measures the same phenomenon, those sensors being of the same type, a combination of, or another type of sensor not disclosed, so that in the event one sensor fails, the ability of system  200  and/or a user to detect phenomenon is maintained and in a non-limiting example, a user alter aircraft usage pursuant to sensor readings. 
     Still referring to  FIG.  2   , sensor  216  may include a humidity sensor. Humidity, as used in this disclosure, is the property of a gaseous medium (almost always air) to hold water in the form of vapor. An amount of water vapor contained within a parcel of air can vary significantly. Water vapor is generally invisible to the human eye and may be damaging to electrical components. There are three primary measurements of humidity, absolute, relative, specific humidity. “Absolute humidity,” for the purposes of this disclosure, describes the water content of air and is expressed in either grams per cubic meters or grams per kilogram. “Relative humidity”, for the purposes of this disclosure, is expressed as a percentage, indicating a present stat of absolute humidity relative to a maximum humidity given the same temperature. “Specific humidity”, for the purposes of this disclosure, is the ratio of water vapor mass to total moist air parcel mass, where parcel is a given portion of a gaseous medium. A humidity sensor may include a psychrometer. A humidity sensor may include a hygrometer. A humidity sensor may be configured to act as or include a humidistat. A “humidistat”, for the purposes of this disclosure, is a humidity-triggered switch, often used to control another electronic device. A humidity sensor may use capacitance to measure relative humidity and include in itself, or as an external component, include a device to convert relative humidity measurements to absolute humidity measurements. “Capacitance”, for the purposes of this disclosure, is the ability of a system to store an electric charge, in this case the system is a parcel of air which may be near, adjacent to, or above a battery cell. 
     With continued reference to  FIG.  2   , sensor  216  may include a multimeter. A multimeter may be configured to measure voltage across a component, electrical current through a component, and resistance of a component. A multimeter may include separate sensors to measure each of the previously disclosed electrical characteristics such as voltmeter, ammeter, and ohmmeter, respectively. 
     Alternatively or additionally, and with continued reference to  FIG.  2   , sensor  216  may include a sensor or plurality thereof that may detect voltage and direct the charging of individual battery cells according to charge level; detection may be performed using any suitable component, set of components, and/or mechanism for direct or indirect measurement and/or detection of voltage levels, including without limitation comparators, analog to digital converters, any form of voltmeter, or the like. Sensor  216  and/or a control circuit incorporated therein and/or communicatively connected thereto may be configured to adjust charge to one or more battery cells as a function of a charge level and/or a detected parameter. For instance, and without limitation, sensor  216  may be configured to determine that a charge level of a battery cell is high based on a detected voltage level of that battery cell or portion of the battery pack. Sensor  216  may alternatively or additionally detect a charge reduction event, defined for purposes of this disclosure as any temporary or permanent state of a battery cell requiring reduction or cessation of charging; a charge reduction event may include a cell being fully charged and/or a cell undergoing a physical and/or electrical process that makes continued charging at a current voltage and/or current level inadvisable due to a risk that the cell will be damaged, will overheat, or the like. Detection of a charge reduction event may include detection of a temperature, of the cell above a threshold level, detection of a voltage and/or resistance level above or below a threshold, or the like. Sensor  216  may include digital sensors, analog sensors, or a combination thereof. Sensor  216  may include digital-to-analog converters (DAC), analog-to-digital converters (ADC, A/D, A-to-D), a combination thereof. 
     With continued reference to  FIG.  2   , sensor  216  may include thermocouples, thermistors, thermometers, passive infrared sensors, resistance temperature sensors (RTD&#39;s), semiconductor based integrated circuits (IC), a combination thereof or another undisclosed sensor type, alone or in combination. Temperature, for the purposes of this disclosure, and as would be appreciated by someone of ordinary skill in the art, is a measure of the heat energy of a system. Temperature, as measured by any number or combinations of sensors present within sensor  216 , may be measured in Fahrenheit (° F.), Celsius (° C.), Kelvin (° K), or another scale alone or in combination. A temperature measured by sensors may comprise electrical signals which are transmitted to their appropriate destination wireless or through a wired connection. 
     With continued reference to  FIG.  2   , sensor  216  may include a sensor configured to detect gas that may be emitted during or after a catastrophic cell failure. “Catastrophic cell failure”, for the purposes of this disclosure, refers to a malfunction of a battery cell, which may be an electrochemical cell, that renders the cell inoperable for its designed function, namely providing electrical energy to at least a portion of an electric aircraft. Byproducts of catastrophic cell failure may include gaseous discharge including oxygen, hydrogen, carbon dioxide, methane, carbon monoxide, a combination thereof, or another undisclosed gas, alone or in combination. Further, sensor  216  may be configured to detect vent gas from electrochemical cells that may comprise a gas detector. For the purposes of this disclosure, a “gas detector” is a device used to detect a gas is present in an area. Gas detectors, and more specifically, the gas sensor that may be used in sensor  216 , may be configured to detect combustible, flammable, toxic, oxygen depleted, a combination thereof, or another type of gas alone or in combination. A gas sensor that may be present in sensor  216  may include a combustible gas, photoionization detectors, electrochemical gas sensors, ultrasonic sensors, metal-oxide-semiconductor (MOS) sensors, infrared imaging sensors, a combination thereof, or another undisclosed type of gas sensor alone or in combination. Sensor  216  may include sensors that are configured to detect non-gaseous byproducts of catastrophic cell failure including, in non-limiting examples, liquid chemical leaks including aqueous alkaline solution, ionomer, molten phosphoric acid, liquid electrolytes with redox shuttle and ionomer, and salt water, among others. Sensor  216  may include sensors that are configured to detect non-gaseous byproducts of catastrophic cell failure including, in non-limiting examples, electrical anomalies as detected by any of the previous disclosed sensors or components. 
     Still referring to  FIG.  2   , electric aircraft  204  may include computing device  220 . Computing device  220  may be in electrical communication with sensor  216 . In some embodiments, computing device  220  may be configured to receive battery data from sensor  216  through a wired connection. In other embodiments, computing device  220  may be configured to receive data from sensor  216  through a wireless connection “Battery data” as used in this disclosure is any information relating to one or more battery cells. In some embodiments, battery data may include, but is not limited to, temperature, voltage, current, capacity, health, humidity, pressure, and the like. In some embodiments, computing device  220  may determine a battery data threshold. A “battery data threshold” as used in this disclosure is any minimum or maximum value of a metric relating to one or more battery cells. In a non-limiting example, a battery data threshold may include a maximum temperature of battery cells  208 . In some embodiments, computing device  220  may be configured to operate vents  212  as a function of battery data received from sensor  216 . Computing device  220  may activate one or more movable components of vents  212  to adjust a position, orientation, and the like of vents  212 . Computing device  212  may adjust vents  212  which may adjust a conductive pathway of battery cells  208 . A “conductive pathway” as used in this disclosure is any path of a medium travelling through one or more battery cells. In some embodiments, computing device  212  may adjust vents  212  to allow an open conductive pathway throughout each battery of battery cells  208 . An open conductive pathway may allow for cool air to flow through battery cells  208 , which may reduce a temperature of battery cells  208 . In some embodiments, an open conductive pathway may allow for heated air to flow away from battery cells  208 . In some embodiments, an open conductive pathway may allow for heated air to flow towards battery cells  208 , which may increase a temperature of battery cells  208 . In a non-limiting example, battery cells  208  may have a temperature beneath ideal operating conditions. Computing device  220  may adjust vents  212  to allow heated air to travel through an open conductive pathway to heat battery cells  208 . In some embodiments, computing device  220  may adjust a vent of vents  212  to warm or cool an individual battery of battery cells  208 . Computing device  220  may include a flight controller as described below with reference to  FIG.  4   . 
     Still referring to  FIG.  2   , computing device  220  may be configured to generate vent arrangement  224 . A “vent arrangement” as used in this disclosure is any positioning of two or more vents. In some embodiments, computing device  220  may be configured to determine a vent arrangement as a function of battery data received from sensor  216 . A vent arrangement may include multiple orientations of vents  212 . As a non-limiting example, a first vent of a first battery cell may be in a closed position. A second vent of a second battery cell may be in an open position. In this example, the first battery cell may remain unchanged while the second battery cell may have a reduction in temperature. In some embodiments, vent arrangement  224  may denote that a plurality of vents may interact with a battery cell of battery cells  208 . In a non-limiting example, vent arrangement  224  may have a first vent of a first battery cell and a second vent of a second battery cell both directed towards the first battery cell. In some embodiments, vent arrangement  224  may include rotational angles of vents  212 . In some embodiments, vent arrangement may include one or more vents of vents  212  positioned at a 45° angle. Computing device  220  may utilize a machine-learning model to predict an optimal vent arrangement  224 . A machine-learning model may be trained on training data correlating battery data to a vent arrangement. Training data may be received from previous venting operations. In some embodiments, training data may be received from user input of computing device  220 . In some embodiments, computing device  220  may utilize a machine-learning model to input a plurality of battery data from sensor  216  and generate vent arrangement  224 . A machine learning model may be described in further detail below with reference to  FIG.  5   . 
     Referring now to  FIG.  3   , vent arrangement  300  is shown. Vent arrangement  300  may include battery modules  304 A-D. Battery modules  304 A-D may include battery cells as described above with reference to  FIG.  2   . Battery modules  304 A-D may include conductive tabs  308 A-D. Conductive tabs  308 A-D may be configured to extend a conductive path throughout battery modules  340 A-D. In some embodiments, conductive tabs  308 A-D may be positioned on a bottom side of battery modules  304 A-D. In some embodiments, conductive tabs  308 A-D may be positioned in a rear, top, side, or front placement of battery modules  304 A-D. Vent arrangement  300  may include vents  312 A-D. Vents  312 A-D may be placed on a bottom, rear, top, side, and/or front placement of battery modules  304 A-D. In some embodiments, vents  312 A-D may be placed by conductive tabs  308 A-D. In some embodiments, vent arrangement  300  may include pathway  316 . Pathway  316  may include a direction of a flow of a medium throughout battery modules  304 A-D. In some embodiments, pathway  316  may include a horizontal direction going left to right. In other embodiments, pathway  316  may include a horizontal direction going right to left. In some embodiments, pathway  316  may include a vertical direction going top to bottom. In some embodiments, pathway  316  may include a vertical direction going bottom to top. In some embodiments, pathway  316  may include any orientation of any direction and/or angle. 
     Still referring to  FIG.  3   , pathway  316  may be adjusted to interact with battery modules  304 A-D based on a configuration of vents  312 A-D. In some embodiments, vent  312 A may be positioned to prevent pathway  316  from interacting with battery module  304 B. Vent  312 B may be positioned to allow pathway  316  to interact with battery module  304 C. Vent  312 C may be positioned to prevent pathway  316  from interacting with battery module  304 D. Vent  312 D may be positioned to prevent pathway  316  from interacting with another battery module. In some embodiments, vents  312 A-D may be adjusted in real time. In a non-limiting example, battery module  304 C may be determined to be overheating. Vent  312 B may be positioned at an upwards angle to allow pathway  316  to interact with battery module  304 C. Vent  312 C may also be positioned in an open configuration to allow more interaction of battery module  304 C and pathway  316 . Vents  312 A-D may be positioned in any orientation and/or angle to allow or prevent pathway  316  from interacting with any number of battery modules  304 A-D. 
     Referring now to  FIG.  4   , an embodiment of battery management component system  400  is presented. Battery management component system  400  may be configured to communicate with computing device  220  of battery ventilation system  200 . In some embodiments, battery management component system  400  may be configured to communicate battery data to computing device  220 . Computing device  220  may adjust vent arrangement  224  as a function of battery data received from battery management system  400 . 
     Still referring to  FIG.  4   , battery management system  400  is to be integrated in a battery pack configured for use in an electric aircraft. The battery management system  400  is to be integrated in a portion of the battery pack or subassembly thereof, which will be disclosed with further detail with reference to  FIG.  3   . Battery management system  400  includes first battery management component  404  disposed on a first end of the battery pack. One of ordinary skill in the art will appreciate that there are various areas in and on a battery pack and/or subassemblies thereof that may include first battery management component  404 . First battery management component  404  may take any suitable form. In a non-limiting embodiment, first battery management component  104  may include a circuit board, such as a printed circuit board and/or integrated circuit board, a subassembly mechanically coupled to at least a portion of the battery pack, standalone components communicatively coupled together, or another undisclosed arrangement of components; for instance, and without limitation, a number of components of first battery management component  404  may be soldered or otherwise electrically connected to a circuit board. First battery management component may be disposed directly over, adjacent to, facing, and/or near a battery module and specifically at least a portion of a battery cell, the arrangement of which will be disclosed with greater detail in reference to  FIG.  3   . First battery management component  404  includes first sensor suite  408 . First sensor suite  408  is configured to measure, detect, sense, and transmit first plurality of battery pack data  428  to data storage system  420 , which will be disclosed in further detail with reference to  FIG.  5   . 
     Referring again to  FIG.  4   , battery management system  400  includes second battery management component  412 . Second battery management component  412  is disposed in or on a second end of battery pack  424 . Second battery management component  412  includes second sensor suite  416 . Second sensor suite  416  may be consistent with the description of any sensor suite disclosed herein. Second sensor suite  416  is configured to measure second plurality of battery pack data  432 . Second plurality of battery pack data  432  may be consistent with the description of any battery pack data disclosed herein. Second plurality of battery pack data  432  may additionally or alternatively include data not measured or recorded in another section of battery management system  400 . Second plurality of battery pack data  432  may be communicated to additional or alternate systems to which it is communicatively coupled. Second sensor suite  416  includes a humidity sensor consistent with any humidity sensor disclosed herein, namely humidity sensor  204 . 
     With continued reference to  FIG.  4   , first battery management component  404  disposed in or on battery pack  424  may be physically isolated from second battery management component  412  also disposed on or in battery pack  424 . “Physical isolation”, for the purposes of this disclosure, refer to a first system&#39;s components, communicative coupling, and any other constituent parts, whether software or hardware, are separated from a second system&#39;s components, communicative coupling, and any other constituent parts, whether software or hardware, respectively. First battery management component  404  and second battery management component  408  may perform the same or different functions in battery management system  400 . In a non-limiting embodiment, the first and second battery management components perform the same, and therefore redundant functions. If, for example, first battery management component  404  malfunctions, in whole or in part, second battery management component  408  may still be operating properly and therefore battery management system  400  may still operate and function properly for electric aircraft in which it is installed. Additionally or alternatively, second battery management component  408  may power on while first battery management component  404  is malfunctioning. One of ordinary skill in the art would understand that the terms “first” and “second” do not refer to either “battery management components” as primary or secondary. In non-limiting embodiments, first battery management component  404  and second battery management component  408  may be powered on and operate through the same ground operations of an electric aircraft and through the same flight envelope of an electric aircraft. This does not preclude one battery management component, first battery management component  404 , from taking over for second battery management component  408  if it were to malfunction. In non-limiting embodiments, the first and second battery management components, due to their physical isolation, may be configured to withstand malfunctions or failures in the other system and survive and operate. Provisions may be made to shield first battery management component  404  from second battery management component  408  other than physical location such as structures and circuit fuses. In non-limiting embodiments, first battery management component  404 , second battery management component  408 , or subcomponents thereof may be disposed on an internal component or set of components within battery pack  424 , such as on battery module sense board  220 . 
     Referring again to  FIG.  4   , first battery management component  404  may be electrically isolated from second battery management component  408 . “Electrical isolation”, for the purposes of this disclosure, refer to a first system&#39;s separation of components carrying electrical signals or electrical energy from a second system&#39;s components. First battery management component  404  may suffer an electrical catastrophe, rendering it inoperable, and due to electrical isolation, second battery management component  408  may still continue to operate and function normally, managing the battery pack of an electric aircraft. Shielding such as structural components, material selection, a combination thereof, or another undisclosed method of electrical isolation and insulation may be used, in non-limiting embodiments. For example, a rubber or other electrically insulating material component may be disposed between the electrical components of the first and second battery management components preventing electrical energy to be conducted through it, isolating the first and second battery management components from each other. 
     With continued reference to  FIG.  4   , battery management system  400  includes data storage system  420 . Data storage system  420  is configured to store first plurality of battery pack data  428  and second plurality of battery pack data  432 . Data storage system  420  may include a database. Data storage system  420  may include a solid-state memory or tape hard drive. Data storage system  420  may be communicatively coupled to first battery management component  404  and second battery management component  412  and may be configured to receive electrical signals related to physical or electrical phenomenon measured and store those electrical signals as first battery pack data  428  and second battery pack data  432 , respectively. Alternatively, data storage system  120  may include more than one discrete data storage systems that are physically and electrically isolated from each other. In this non-limiting embodiment, each of first battery management component  404  and second battery management component  412  may store first battery pack data  428  and second battery pack data  432  separately. One of ordinary skill in the art would understand the virtually limitless arrangements of data stores with which battery management system  400  could employ to store the first and second plurality of battery pack data. 
     Referring again to  FIG.  4   , data storage system  420  stores first plurality of battery pack data  428  and second plurality of battery pack data  432 . First plurality of battery pack data  428  and second plurality of battery pack data  432  may include total flight hours that battery pack  424  and/or electric aircraft have been operating. The first and second plurality of battery pack data may include total energy flowed through battery pack  424 . Data storage system  420  may be communicatively coupled to sensors that detect, measure and store energy in a plurality of measurements which may include current, voltage, resistance, impedance, coulombs, watts, temperature, or a combination thereof. Additionally or alternatively, data storage system  420  may be communicatively coupled to a sensor suite consistent with this disclosure to measure physical and/or electrical characteristics. Data storage system  420  may be configured to store first battery pack data  428  and second battery pack data  432  wherein at least a portion of the data includes battery pack maintenance history. Battery pack maintenance history may include mechanical failures and technician resolutions thereof, electrical failures and technician resolutions thereof. Additionally, battery pack maintenance history may include component failures such that the overall system still functions. Data storage system  420  may store the first and second battery pack data that includes an upper voltage threshold and lower voltage threshold consistent with this disclosure. First battery pack data  428  and second battery pack data  432  may include a moisture level threshold. The moisture level threshold may include an absolute, relative, and/or specific moisture level threshold. 
     Referring now to  FIG.  5   , an exemplary embodiment  500  of a flight controller  504  is illustrated. As used in this disclosure a “flight controller” is a computing device of a plurality of computing devices dedicated to data storage, security, distribution of traffic for load balancing, and flight instruction. Flight controller  504  may include and/or communicate with any computing device as described in this disclosure, including without limitation a microcontroller, microprocessor, digital signal processor (DSP) and/or system on a chip (SoC) as described in this disclosure. Further, flight controller  504  may include a single computing device operating independently, or may include two or more computing device operating in concert, in parallel, sequentially or the like; two or more computing devices may be included together in a single computing device or in two or more computing devices. In embodiments, flight controller  404  may be installed in an aircraft, may control the aircraft remotely, and/or may include an element installed in the aircraft and a remote element in communication therewith. 
     In an embodiment, and still referring to  FIG.  5   , flight controller  504  may include a signal transformation component  508 . As used in this disclosure a “signal transformation component” is a component that transforms and/or converts a first signal to a second signal, wherein a signal may include one or more digital and/or analog signals. For example, and without limitation, signal transformation component  508  may be configured to perform one or more operations such as preprocessing, lexical analysis, parsing, semantic analysis, and the like thereof. In an embodiment, and without limitation, signal transformation component  508  may include one or more analog-to-digital convertors that transform a first signal of an analog signal to a second signal of a digital signal. For example, and without limitation, an analog-to-digital converter may convert an analog input signal to a 10-bit binary digital representation of that signal. In another embodiment, signal transformation component  508  may include transforming one or more low-level languages such as, but not limited to, machine languages and/or assembly languages. For example, and without limitation, signal transformation component  508  may include transforming a binary language signal to an assembly language signal. In an embodiment, and without limitation, signal transformation component  508  may include transforming one or more high-level languages and/or formal languages such as but not limited to alphabets, strings, and/or languages. For example, and without limitation, high-level languages may include one or more system languages, scripting languages, domain-specific languages, visual languages, esoteric languages, and the like thereof. As a further non-limiting example, high-level languages may include one or more algebraic formula languages, business data languages, string and list languages, object-oriented languages, and the like thereof 
     Still referring to  FIG.  4   , signal transformation component  508  may be configured to optimize an intermediate representation  512 . As used in this disclosure an “intermediate representation” is a data structure and/or code that represents the input signal. Signal transformation component  408  may optimize intermediate representation as a function of a data-flow analysis, dependence analysis, alias analysis, pointer analysis, escape analysis, and the like thereof. In an embodiment, and without limitation, signal transformation component  508  may optimize intermediate representation  512  as a function of one or more inline expansions, dead code eliminations, constant propagation, loop transformations, and/or automatic parallelization functions. In another embodiment, signal transformation component  508  may optimize intermediate representation as a function of a machine dependent optimization such as a peephole optimization, wherein a peephole optimization may rewrite short sequences of code into more efficient sequences of code. Signal transformation component  508  may optimize intermediate representation to generate an output language, wherein an “output language,” as used herein, is the native machine language of flight controller  504 . For example, and without limitation, native machine language may include one or more binary and/or numerical languages. 
     In an embodiment, and without limitation, signal transformation component  508  may include transform one or more inputs and outputs as a function of an error correction code. An error correction code, also known as error correcting code (ECC), is an encoding of a message or lot of data using redundant information, permitting recovery of corrupted data. An ECC may include a block code, in which information is encoded on fixed-size packets and/or blocks of data elements such as symbols of predetermined size, bits, or the like. Reed-Solomon coding, in which message symbols within a symbol set having q symbols are encoded as coefficients of a polynomial of degree less than or equal to a natural number k, over a finite field F with q elements; strings so encoded have a minimum hamming distance of k+1, and permit correction of (q−k−1)/2 erroneous symbols. Block code may alternatively or additionally be implemented using Golay coding, also known as binary Golay coding, Bose-Chaudhuri, Hocquenghuem (BCH) coding, multidimensional parity-check coding, and/or Hamming codes. An ECC may alternatively or additionally be based on a convolutional code. 
     In an embodiment, and still referring to  FIG.  4   , flight controller  504  may include a reconfigurable hardware platform  516 . A “reconfigurable hardware platform,” as used herein, is a component and/or unit of hardware that may be reprogrammed, such that, for instance, a data path between elements such as logic gates or other digital circuit elements may be modified to change an algorithm, state, logical sequence, or the like of the component and/or unit. This may be accomplished with such flexible high-speed computing fabrics as field-programmable gate arrays (FPGAs), which may include a grid of interconnected logic gates, connections between which may be severed and/or restored to program in modified logic. Reconfigurable hardware platform  416  may be reconfigured to enact any algorithm and/or algorithm selection process received from another computing device and/or created using machine-learning processes. 
     Still referring to  FIG.  4   , reconfigurable hardware platform  516  may include a logic component  520 . As used in this disclosure a “logic component” is a component that executes instructions on output language. For example, and without limitation, logic component may perform basic arithmetic, logic, controlling, input/output operations, and the like thereof. Logic component  520  may include any suitable processor, such as without limitation a component incorporating logical circuitry for performing arithmetic and logical operations, such as an arithmetic and logic unit (ALU), which may be regulated with a state machine and directed by operational inputs from memory and/or sensors; logic component  520  may be organized according to Von Neumann and/or Harvard architecture as a non-limiting example. Logic component  520  may include, incorporate, and/or be incorporated in, without limitation, a microcontroller, microprocessor, digital signal processor (DSP), Field Programmable Gate Array (FPGA), Complex Programmable Logic Device (CPLD), Graphical Processing Unit (GPU), general purpose GPU, Tensor Processing Unit (TPU), analog or mixed signal processor, Trusted Platform Module (TPM), a floating point unit (FPU), and/or system on a chip (SoC). In an embodiment, logic component  520  may include one or more integrated circuit microprocessors, which may contain one or more central processing units, central processors, and/or main processors, on a single metal-oxide-semiconductor chip. Logic component  520  may be configured to execute a sequence of stored instructions to be performed on the output language and/or intermediate representation  512 . Logic component  520  may be configured to fetch and/or retrieve the instruction from a memory cache, wherein a “memory cache,” as used in this disclosure, is a stored instruction set on flight controller  504 . Logic component  520  may be configured to decode the instruction retrieved from the memory cache to opcodes and/or operands. Logic component  520  may be configured to execute the instruction on intermediate representation  512  and/or output language. For example, and without limitation, logic component  520  may be configured to execute an addition operation on intermediate representation  512  and/or output language. 
     In an embodiment, and without limitation, logic component  520  may be configured to calculate a flight element  524 . As used in this disclosure a “flight element” is an element of datum denoting a relative status of aircraft. For example, and without limitation, flight element  524  may denote one or more torques, thrusts, airspeed velocities, forces, altitudes, groundspeed velocities, directions during flight, directions facing, forces, orientations, and the like thereof. For example, and without limitation, flight element  524  may denote that aircraft is cruising at an altitude and/or with a sufficient magnitude of forward thrust. As a further non-limiting example, flight status may denote that is building thrust and/or groundspeed velocity in preparation for a takeoff. As a further non-limiting example, flight element  524  may denote that aircraft is following a flight path accurately and/or sufficiently. 
     Still referring to  FIG.  4   , flight controller  504  may include a chipset component  528 . As used in this disclosure a “chipset component” is a component that manages data flow. In an embodiment, and without limitation, chipset component  528  may include a northbridge data flow path, wherein the northbridge dataflow path may manage data flow from logic component  520  to a high-speed device and/or component, such as a RAM, graphics controller, and the like thereof. In another embodiment, and without limitation, chipset component  528  may include a southbridge data flow path, wherein the southbridge dataflow path may manage data flow from logic component  520  to lower-speed peripheral buses, such as a peripheral component interconnect (PCI), industry standard architecture (ICA), and the like thereof. In an embodiment, and without limitation, southbridge data flow path may include managing data flow between peripheral connections such as ethernet, USB, audio devices, and the like thereof. Additionally or alternatively, chipset component  528  may manage data flow between logic component  520 , memory cache, and a flight component  532 . As used in this disclosure a “flight component” is a portion of an aircraft that can be moved or adjusted to affect one or more flight elements. For example, flight component  532  may include a component used to affect the aircrafts&#39; roll and pitch which may comprise one or more ailerons. As a further example, flight component  532  may include a rudder to control yaw of an aircraft. In an embodiment, chipset component  528  may be configured to communicate with a plurality of flight components as a function of flight element  524 . For example, and without limitation, chipset component  528  may transmit to an aircraft rotor to reduce torque of a first lift propulsor and increase the forward thrust produced by a pusher component to perform a flight maneuver. 
     In an embodiment, and still referring to  FIG.  5   , flight controller  504  may be configured generate an autonomous function. As used in this disclosure an “autonomous function” is a mode and/or function of flight controller  504  that controls aircraft automatically. For example, and without limitation, autonomous function may perform one or more aircraft maneuvers, take offs, landings, altitude adjustments, flight leveling adjustments, turns, climbs, and/or descents. As a further non-limiting example, autonomous function may adjust one or more airspeed velocities, thrusts, torques, and/or groundspeed velocities. As a further non-limiting example, autonomous function may perform one or more flight path corrections and/ or flight path modifications as a function of flight element  524 . In an embodiment, autonomous function may include one or more modes of autonomy such as, but not limited to, autonomous mode, semi-autonomous mode, and/or non-autonomous mode. As used in this disclosure “autonomous mode” is a mode that automatically adjusts and/or controls aircraft and/or the maneuvers of aircraft in its entirety. For example, autonomous mode may denote that flight controller  504  will adjust the aircraft. As used in this disclosure a “semi-autonomous mode” is a mode that automatically adjusts and/or controls a portion and/or section of aircraft. For example, and without limitation, semi-autonomous mode may denote that a pilot will control the propulsors, wherein flight controller  504  will control the ailerons and/or rudders. As used in this disclosure “non-autonomous mode” is a mode that denotes a pilot will control aircraft and/or maneuvers of aircraft in its entirety. 
     In an embodiment, and still referring to  FIG.  5   , flight controller  504  may generate autonomous function as a function of an autonomous machine-learning model. As used in this disclosure an “autonomous machine-learning model” is a machine-learning model to produce an autonomous function output given flight element  524  and a pilot signal  536  as inputs; this is in contrast to a non-machine learning software program where the commands to be executed are determined in advance by a user and written in a programming language. As used in this disclosure a “pilot signal” is an element of datum representing one or more functions a pilot is controlling and/or adjusting. For example, pilot signal  536  may denote that a pilot is controlling and/or maneuvering ailerons, wherein the pilot is not in control of the rudders and/or propulsors. In an embodiment, pilot signal  536  may include an implicit signal and/or an explicit signal. For example, and without limitation, pilot signal  536  may include an explicit signal, wherein the pilot explicitly states there is a lack of control and/or desire for autonomous function. As a further non-limiting example, pilot signal  536  may include an explicit signal directing flight controller  504  to control and/or maintain a portion of aircraft, a portion of the flight plan, the entire aircraft, and/or the entire flight plan. As a further non-limiting example, pilot signal  536  may include an implicit signal, wherein flight controller  504  detects a lack of control such as by a malfunction, torque alteration, flight path deviation, and the like thereof. In an embodiment, and without limitation, pilot signal  536  may include one or more explicit signals to reduce torque, and/or one or more implicit signals that torque may be reduced due to reduction of airspeed velocity. In an embodiment, and without limitation, pilot signal  536  may include one or more local and/or global signals. For example, and without limitation, pilot signal  536  may include a local signal that is transmitted by a pilot and/or crew member. As a further non-limiting example, pilot signal  536  may include a global signal that is transmitted by air traffic control and/or one or more remote users that are in communication with the pilot of aircraft. In an embodiment, pilot signal  536  may be received as a function of a tri-state bus and/or multiplexor that denotes an explicit pilot signal should be transmitted prior to any implicit or global pilot signal. 
     Still referring to  FIG.  5   , autonomous machine-learning model may include one or more autonomous machine-learning processes such as supervised, unsupervised, or reinforcement machine-learning processes that flight controller  504  and/or a remote device may or may not use in the generation of autonomous function. As used in this disclosure “remote device” is an external device to flight controller  504 . Additionally or alternatively, autonomous machine-learning model may include one or more autonomous machine-learning processes that a field-programmable gate array (FPGA) may or may not use in the generation of autonomous function. Autonomous machine-learning process may include, without limitation machine learning processes such as simple linear regression, multiple linear regression, polynomial regression, support vector regression, ridge regression, lasso regression, elasticnet regression, decision tree regression, random forest regression, logistic regression, logistic classification, K-nearest neighbors, support vector machines, kernel support vector machines, naive bayes, decision tree classification, random forest classification, K-means clustering, hierarchical clustering, dimensionality reduction, principal component analysis, linear discriminant analysis, kernel principal component analysis, Q-learning, State Action Reward State Action (SARSA), Deep-Q network, Markov decision processes, Deep Deterministic Policy Gradient (DDPG), or the like thereof. 
     In an embodiment, and still referring to  FIG.  5   , autonomous machine learning model may be trained as a function of autonomous training data, wherein autonomous training data may correlate a flight element, pilot signal, and/or simulation data to an autonomous function. For example, and without limitation, a flight element of an airspeed velocity, a pilot signal of limited and/or no control of propulsors, and a simulation data of required airspeed velocity to reach the destination may result in an autonomous function that includes a semi-autonomous mode to increase thrust of the propulsors. Autonomous training data may be received as a function of user-entered valuations of flight elements, pilot signals, simulation data, and/or autonomous functions. Flight controller  404  may receive autonomous training data by receiving correlations of flight element, pilot signal, and/or simulation data to an autonomous function that were previously received and/or determined during a previous iteration of generation of autonomous function. Autonomous training data may be received by one or more remote devices and/or FPGAs that at least correlate a flight element, pilot signal, and/or simulation data to an autonomous function. Autonomous training data may be received in the form of one or more user-entered correlations of a flight element, pilot signal, and/or simulation data to an autonomous function. 
     Still referring to  FIG.  5   , flight controller  504  may receive autonomous machine-learning model from a remote device and/or FPGA that utilizes one or more autonomous machine learning processes, wherein a remote device and an FPGA is described above in detail. For example, and without limitation, a remote device may include a computing device, external device, processor, FPGA, microprocessor and the like thereof. Remote device and/or FPGA may perform the autonomous machine-learning process using autonomous training data to generate autonomous function and transmit the output to flight controller  504 . Remote device and/or FPGA may transmit a signal, bit, datum, or parameter to flight controller  504  that at least relates to autonomous function. Additionally or alternatively, the remote device and/or FPGA may provide an updated machine-learning model. For example, and without limitation, an updated machine-learning model may be comprised of a firmware update, a software update, an autonomous machine-learning process correction, and the like thereof. As a non-limiting example a software update may incorporate a new simulation data that relates to a modified flight element. Additionally or alternatively, the updated machine learning model may be transmitted to the remote device and/or FPGA, wherein the remote device and/or FPGA may replace the autonomous machine-learning model with the updated machine-learning model and generate the autonomous function as a function of the flight element, pilot signal, and/or simulation data using the updated machine-learning model. The updated machine-learning model may be transmitted by the remote device and/or FPGA and received by flight controller  504  as a software update, firmware update, or corrected autonomous machine-learning model. For example, and without limitation autonomous machine learning model may utilize a neural net machine-learning process, wherein the updated machine-learning model may incorporate a gradient boosting machine-learning process. 
     Still referring to  FIG.  5   , flight controller  504  may include, be included in, and/or communicate with a mobile device such as a mobile telephone or smartphone. Further, flight controller may communicate with one or more additional devices as described below in further detail via a network interface device. The network interface device may be utilized for commutatively connecting a flight controller to one or more of a variety of networks, and one or more devices. Examples of a network interface device include, but are not limited to, a network interface card (e.g., a mobile network interface card, a LAN card), a modem, and any combination thereof. Examples of a network include, but are not limited to, a wide area network (e.g., the Internet, an enterprise network), a local area network (e.g., a network associated with an office, a building, a campus or other relatively small geographic space), a telephone network, a data network associated with a telephone/voice provider (e.g., a mobile communications provider data and/or voice network), a direct connection between two computing devices, and any combinations thereof. The network may include any network topology and can may employ a wired and/or a wireless mode of communication. 
     In an embodiment, and still referring to  FIG.  5   , flight controller  504  may include, but is not limited to, for example, a cluster of flight controllers in a first location and a second flight controller or cluster of flight controllers in a second location. Flight controller  504  may include one or more flight controllers dedicated to data storage, security, distribution of traffic for load balancing, and the like. Flight controller  504  may be configured to distribute one or more computing tasks as described below across a plurality of flight controllers, which may operate in parallel, in series, redundantly, or in any other manner used for distribution of tasks or memory between computing devices. For example, and without limitation, flight controller  504  may implement a control algorithm to distribute and/or command the plurality of flight controllers. As used in this disclosure a “control algorithm” is a finite sequence of well-defined computer implementable instructions that may determine the flight component of the plurality of flight components to be adjusted. For example, and without limitation, control algorithm may include one or more algorithms that reduce and/or prevent aviation asymmetry. As a further non-limiting example, control algorithms may include one or more models generated as a function of a software including, but not limited to Simulink by MathWorks, Natick, Mass., USA. In an embodiment, and without limitation, control algorithm may be configured to generate an auto-code, wherein an “auto-code,” is used herein, is a code and/or algorithm that is generated as a function of the one or more models and/or software&#39;s. In another embodiment, control algorithm may be configured to produce a segmented control algorithm. As used in this disclosure a “segmented control algorithm” is control algorithm that has been separated and/or parsed into discrete sections. For example, and without limitation, segmented control algorithm may parse control algorithm into two or more segments, wherein each segment of control algorithm may be performed by one or more flight controllers operating on distinct flight components. 
     In an embodiment, and still referring to  FIG.  5   , control algorithm may be configured to determine a segmentation boundary as a function of segmented control algorithm. As used in this disclosure a “segmentation boundary” is a limit and/or delineation associated with the segments of the segmented control algorithm. For example, and without limitation, segmentation boundary may denote that a segment in the control algorithm has a first starting section and/or a first ending section. As a further non-limiting example, segmentation boundary may include one or more boundaries associated with an ability of flight component  532 . In an embodiment, control algorithm may be configured to create an optimized signal communication as a function of segmentation boundary. For example, and without limitation, optimized signal communication may include identifying the discrete timing required to transmit and/or receive the one or more segmentation boundaries. In an embodiment, and without limitation, creating optimized signal communication further comprises separating a plurality of signal codes across the plurality of flight controllers. For example, and without limitation the plurality of flight controllers may include one or more formal networks, wherein formal networks transmit data along an authority chain and/or are limited to task-related communications. As a further non-limiting example, communication network may include informal networks, wherein informal networks transmit data in any direction. In an embodiment, and without limitation, the plurality of flight controllers may include a chain path, wherein a “chain path,” as used herein, is a linear communication path comprising a hierarchy that data may flow through. In an embodiment, and without limitation, the plurality of flight controllers may include an all-channel path, wherein an “all-channel path,” as used herein, is a communication path that is not restricted to a particular direction. For example, and without limitation, data may be transmitted upward, downward, laterally, and the like thereof. In an embodiment, and without limitation, the plurality of flight controllers may include one or more neural networks that assign a weighted value to a transmitted datum. For example, and without limitation, a weighted value may be assigned as a function of one or more signals denoting that a flight component is malfunctioning and/or in a failure state. 
     Still referring to  FIG.  5   , the plurality of flight controllers may include a master bus controller. As used in this disclosure a “master bus controller” is one or more devices and/or components that are connected to a bus to initiate a direct memory access transaction, wherein a bus is one or more terminals in a bus architecture. Master bus controller may communicate using synchronous and/or asynchronous bus control protocols. In an embodiment, master bus controller may include flight controller  504 . In another embodiment, master bus controller may include one or more universal asynchronous receiver-transmitters (UART). For example, and without limitation, master bus controller may include one or more bus architectures that allow a bus to initiate a direct memory access transaction from one or more buses in the bus architectures. As a further non-limiting example, master bus controller may include one or more peripheral devices and/or components to communicate with another peripheral device and/or component and/or the master bus controller. In an embodiment, master bus controller may be configured to perform bus arbitration. As used in this disclosure “bus arbitration” is method and/or scheme to prevent multiple buses from attempting to communicate with and/or connect to master bus controller. For example and without limitation, bus arbitration may include one or more schemes such as a small computer interface system, wherein a small computer interface system is a set of standards for physical connecting and transferring data between peripheral devices and master bus controller by defining commands, protocols, electrical, optical, and/or logical interfaces. In an embodiment, master bus controller may receive intermediate representation  512  and/or output language from logic component  520 , wherein output language may include one or more analog-to-digital conversions, low bit rate transmissions, message encryptions, digital signals, binary signals, logic signals, analog signals, and the like thereof described above in detail. 
     Still referring to  FIG.  5   , master bus controller may communicate with a slave bus. As used in this disclosure a “slave bus” is one or more peripheral devices and/or components that initiate a bus transfer. For example, and without limitation, slave bus may receive one or more controls and/or asymmetric communications from master bus controller, wherein slave bus transfers data stored to master bus controller. In an embodiment, and without limitation, slave bus may include one or more internal buses, such as but not limited to a/an internal data bus, memory bus, system bus, front-side bus, and the like thereof. In another embodiment, and without limitation, slave bus may include one or more external buses such as external flight controllers, external computers, remote devices, printers, aircraft computer systems, flight control systems, and the like thereof. 
     In an embodiment, and still referring to  FIG.  5   , control algorithm may optimize signal communication as a function of determining one or more discrete timings. For example, and without limitation master bus controller may synchronize timing of the segmented control algorithm by injecting high priority timing signals on a bus of the master bus control. As used in this disclosure a “high priority timing signal” is information denoting that the information is important. For example, and without limitation, high priority timing signal may denote that a section of control algorithm is of high priority and should be analyzed and/or transmitted prior to any other sections being analyzed and/or transmitted. In an embodiment, high priority timing signal may include one or more priority packets. As used in this disclosure a “priority packet” is a formatted unit of data that is communicated between the plurality of flight controllers. For example, and without limitation, priority packet may denote that a section of control algorithm should be used and/or is of greater priority than other sections. 
     Still referring to  FIG.  5   , flight controller  504  may also be implemented using a “shared nothing” architecture in which data is cached at the worker, in an embodiment, this may enable scalability of aircraft and/or computing device. Flight controller  504  may include a distributer flight controller. As used in this disclosure a “distributer flight controller” is a component that adjusts and/or controls a plurality of flight components as a function of a plurality of flight controllers. For example, distributer flight controller may include a flight controller that communicates with a plurality of additional flight controllers and/or clusters of flight controllers. In an embodiment, distributed flight control may include one or more neural networks. For example, neural network also known as an artificial neural network, is a network of “nodes,” or data structures having one or more inputs, one or more outputs, and a function determining outputs based on inputs. Such nodes may be organized in a network, such as without limitation a convolutional neural network, including an input layer of nodes, one or more intermediate layers, and an output layer of nodes. Connections between nodes may be created via the process of “training” the network, in which elements from a training dataset are applied to the input nodes, a suitable training algorithm (such as Levenberg-Marquardt, conjugate gradient, simulated annealing, or other algorithms) is then used to adjust the connections and weights between nodes in adjacent layers of the neural network to produce the desired values at the output nodes. This process is sometimes referred to as deep learning. 
     Still referring to  FIG.  5   , a node may include, without limitation a plurality of inputs xi that may receive numerical values from inputs to a neural network containing the node and/or from other nodes. Node may perform a weighted sum of inputs using weights w i  that are multiplied by respective inputs x i . Additionally or alternatively, a bias b may be added to the weighted sum of the inputs such that an offset is added to each unit in the neural network layer that is independent of the input to the layer. The weighted sum may then be input into a function φ, which may generate one or more outputs y. Weight w i  applied to an input x i  may indicate whether the input is “excitatory,” indicating that it has strong influence on the one or more outputs y, for instance by the corresponding weight having a large numerical value, and/or a “inhibitory,” indicating it has a weak effect influence on the one more inputs y, for instance by the corresponding weight having a small numerical value. The values of weights w i  may be determined by training a neural network using training data, which may be performed using any suitable process as described above. In an embodiment, and without limitation, a neural network may receive semantic units as inputs and output vectors representing such semantic units according to weights w i  that are derived using machine-learning processes as described in this disclosure. 
     Still referring to  FIG.  5   , flight controller may include a sub-controller  540 . As used in this disclosure a “sub-controller” is a controller and/or component that is part of a distributed controller as described above; for instance, flight controller  504  may be and/or include a distributed flight controller made up of one or more sub-controllers. For example, and without limitation, sub-controller  540  may include any controllers and/or components thereof that are similar to distributed flight controller and/or flight controller as described above. Sub-controller  540  may include any component of any flight controller as described above. Sub-controller  540  may be implemented in any manner suitable for implementation of a flight controller as described above. As a further non-limiting example, sub-controller  540  may include one or more processors, logic components and/or computing devices capable of receiving, processing, and/or transmitting data across the distributed flight controller as described above. As a further non-limiting example, sub-controller  540  may include a controller that receives a signal from a first flight controller and/or first distributed flight controller component and transmits the signal to a plurality of additional sub-controllers and/or flight components. 
     Still referring to  FIG.  5   , flight controller may include a co-controller  544 . As used in this disclosure a “co-controller” is a controller and/or component that joins flight controller  504  as components and/or nodes of a distributer flight controller as described above. For example, and without limitation, co-controller  544  may include one or more controllers and/or components that are similar to flight controller  504 . As a further non-limiting example, co-controller  544  may include any controller and/or component that joins flight controller  504  to distributer flight controller. As a further non-limiting example, co-controller  544  may include one or more processors, logic components and/or computing devices capable of receiving, processing, and/or transmitting data to and/or from flight controller  504  to distributed flight control system. Co-controller  544  may include any component of any flight controller as described above. Co-controller  544  may be implemented in any manner suitable for implementation of a flight controller as described above. 
     In an embodiment, and with continued reference to  FIG.  5   , flight controller  504  may be designed and/or configured to perform any method, method step, or sequence of method steps in any embodiment described in this disclosure, in any order and with any degree of repetition. For instance, flight controller  504  may be configured to perform a single step or sequence repeatedly until a desired or commanded outcome is achieved; repetition of a step or a sequence of steps may be performed iteratively and/or recursively using outputs of previous repetitions as inputs to subsequent repetitions, aggregating inputs and/or outputs of repetitions to produce an aggregate result, reduction or decrement of one or more variables such as global variables, and/or division of a larger processing task into a set of iteratively addressed smaller processing tasks. Flight controller may perform any step or sequence of steps as described in this disclosure in parallel, such as simultaneously and/or substantially simultaneously performing a step two or more times using two or more parallel threads, processor cores, or the like; division of tasks between parallel threads and/or processes may be performed according to any protocol suitable for division of tasks between iterations. Persons skilled in the art, upon reviewing the entirety of this disclosure, will be aware of various ways in which steps, sequences of steps, processing tasks, and/or data may be subdivided, shared, or otherwise dealt with using iteration, recursion, and/or parallel processing. 
     Referring now to  FIG.  6   , an exemplary embodiment of a machine-learning module  500  that may perform one or more machine-learning processes as described in this disclosure is illustrated. Machine-learning module may perform determinations, classification, and/or analysis steps, methods, processes, or the like as described in this disclosure using machine learning processes. A “machine learning process,” as used in this disclosure, is a process that automatedly uses training data  604  to generate an algorithm that will be performed by a computing device/module to produce outputs  608  given data provided as inputs  612 ; this is in contrast to a non-machine learning software program where the commands to be executed are determined in advance by a user and written in a programming language. 
     Still referring to  FIG.  6   , “training data,” as used herein, is data containing correlations that a machine-learning process may use to model relationships between two or more categories of data elements. For instance, and without limitation, training data  604  may include a plurality of data entries, each entry representing a set of data elements that were recorded, received, and/or generated together; data elements may be correlated by shared existence in a given data entry, by proximity in a given data entry, or the like. Multiple data entries in training data  604  may evince one or more trends in correlations between categories of data elements; for instance, and without limitation, a higher value of a first data element belonging to a first category of data element may tend to correlate to a higher value of a second data element belonging to a second category of data element, indicating a possible proportional or other mathematical relationship linking values belonging to the two categories. Multiple categories of data elements may be related in training data  604  according to various correlations; correlations may indicate causative and/or predictive links between categories of data elements, which may be modeled as relationships such as mathematical relationships by machine-learning processes as described in further detail below. Training data  604  may be formatted and/or organized by categories of data elements, for instance by associating data elements with one or more descriptors corresponding to categories of data elements. As a non-limiting example, training data  604  may include data entered in standardized forms by persons or processes, such that entry of a given data element in a given field in a form may be mapped to one or more descriptors of categories. Elements in training data  604  may be linked to descriptors of categories by tags, tokens, or other data elements; for instance, and without limitation, training data  604  may be provided in fixed-length formats, formats linking positions of data to categories such as comma-separated value (CSV) formats and/or self-describing formats such as extensible markup language (XML), JavaScript Object Notation (JSON), or the like, enabling processes or devices to detect categories of data. 
     Alternatively or additionally, and continuing to refer to  FIG.  6   , training data  604  may include one or more elements that are not categorized; that is, training data  604  may not be formatted or contain descriptors for some elements of data. Machine-learning algorithms and/or other processes may sort training data  604  according to one or more categorizations using, for instance, natural language processing algorithms, tokenization, detection of correlated values in raw data and the like; categories may be generated using correlation and/or other processing algorithms. As a non-limiting example, in a corpus of text, phrases making up a number “n” of compound words, such as nouns modified by other nouns, may be identified according to a statistically significant prevalence of n-grams containing such words in a particular order; such an n-gram may be categorized as an element of language such as a “word” to be tracked similarly to single words, generating a new category as a result of statistical analysis. Similarly, in a data entry including some textual data, a person&#39;s name may be identified by reference to a list, dictionary, or other compendium of terms, permitting ad-hoc categorization by machine-learning algorithms, and/or automated association of data in the data entry with descriptors or into a given format. The ability to categorize data entries automatedly may enable the same training data  604  to be made applicable for two or more distinct machine-learning algorithms as described in further detail below. Training data  604  used by machine-learning module  600  may correlate any input data as described in this disclosure to any output data as described in this disclosure. As a non-limiting illustrative example inputs may include a plurality of battery data and outputs may include vent arrangements. 
     Further referring to  FIG.  6   , training data may be filtered, sorted, and/or selected using one or more supervised and/or unsupervised machine-learning processes and/or models as described in further detail below; such models may include without limitation a training data classifier  616 . Training data classifier  616  may include a “classifier,” which as used in this disclosure is a machine- learning model as defined below, such as a mathematical model, neural net, or program generated by a machine learning algorithm known as a “classification algorithm,” as described in further detail below, that sorts inputs into categories or bins of data, outputting the categories or bins of data and/or labels associated therewith. A classifier may be configured to output at least a datum that labels or otherwise identifies a set of data that are clustered together, found to be close under a distance metric as described below, or the like. Machine-learning module  600  may generate a classifier using a classification algorithm, defined as a processes whereby a computing device and/or any module and/or component operating thereon derives a classifier from training data  604 . Classification may be performed using, without limitation, linear classifiers such as without limitation logistic regression and/or naive Bayes classifiers, nearest neighbor classifiers such as k-nearest neighbors classifiers, support vector machines, least squares support vector machines, fisher&#39;s linear discriminant, quadratic classifiers, decision trees, boosted trees, random forest classifiers, learning vector quantization, and/or neural network-based classifiers. As a non-limiting example, training data classifier  616  may classify elements of training data to temperatures, voltages, currents, humidity, pressure, and the like. 
     Still referring to  FIG.  6   , machine-learning module  600  may be configured to perform a lazy-learning process  620  and/or protocol, which may alternatively be referred to as a “lazy loading” or “call-when-needed” process and/or protocol, may be a process whereby machine learning is conducted upon receipt of an input to be converted to an output, by combining the input and training set to derive the algorithm to be used to produce the output on demand. For instance, an initial set of simulations may be performed to cover an initial heuristic and/or “first guess” at an output and/or relationship. As a non-limiting example, an initial heuristic may include a ranking of associations between inputs and elements of training data  604 . Heuristic may include selecting some number of highest-ranking associations and/or training data  604  elements. Lazy learning may implement any suitable lazy learning algorithm, including without limitation a K-nearest neighbors algorithm, a lazy naïve Bayes algorithm, or the like; persons skilled in the art, upon reviewing the entirety of this disclosure, will be aware of various lazy-learning algorithms that may be applied to generate outputs as described in this disclosure, including without limitation lazy learning applications of machine-learning algorithms as described in further detail below. 
     Alternatively or additionally, and with continued reference to  FIG.  6   , machine-learning processes as described in this disclosure may be used to generate machine-learning models  624 . A “machine-learning model,” as used in this disclosure, is a mathematical and/or algorithmic representation of a relationship between inputs and outputs, as generated using any machine-learning process including without limitation any process as described above, and stored in memory; an input is submitted to a machine-learning model  624  once created, which generates an output based on the relationship that was derived. For instance, and without limitation, a linear regression model, generated using a linear regression algorithm, may compute a linear combination of input data using coefficients derived during machine-learning processes to calculate an output datum. As a further non-limiting example, a machine-learning model  624  may be generated by creating an artificial neural network, such as a convolutional neural network comprising an input layer of nodes, one or more intermediate layers, and an output layer of nodes. Connections between nodes may be created via the process of “training” the network, in which elements from a training data  604  set are applied to the input nodes, a suitable training algorithm (such as Levenberg-Marquardt, conjugate gradient, simulated annealing, or other algorithms) is then used to adjust the connections and weights between nodes in adjacent layers of the neural network to produce the desired values at the output nodes. This process is sometimes referred to as deep learning. 
     Still referring to  FIG.  6   , machine-learning algorithms may include at least a supervised machine-learning process  628 . At least a supervised machine-learning process  628 , as defined herein, include algorithms that receive a training set relating a number of inputs to a number of outputs, and seek to find one or more mathematical relations relating inputs to outputs, where each of the one or more mathematical relations is optimal according to some criterion specified to the algorithm using some scoring function. For instance, a supervised learning algorithm may include battery data as described above as inputs, vent arrangements as outputs, and a scoring function representing a desired form of relationship to be detected between inputs and outputs; scoring function may, for instance, seek to maximize the probability that a given input and/or combination of elements inputs is associated with a given output to minimize the probability that a given input is not associated with a given output. Scoring function may be expressed as a risk function representing an “expected loss” of an algorithm relating inputs to outputs, where loss is computed as an error function representing a degree to which a prediction generated by the relation is incorrect when compared to a given input-output pair provided in training data  604 . Persons skilled in the art, upon reviewing the entirety of this disclosure, will be aware of various possible variations of at least a supervised machine-learning process  628  that may be used to determine relation between inputs and outputs. Supervised machine-learning processes may include classification algorithms as defined above. 
     Further referring to  FIG.  6   , machine learning processes may include at least an unsupervised machine-learning processes  632 . An unsupervised machine-learning process, as used herein, is a process that derives inferences in datasets without regard to labels; as a result, an unsupervised machine-learning process may be free to discover any structure, relationship, and/or correlation provided in the data. Unsupervised processes may not require a response variable; unsupervised processes may be used to find interesting patterns and/or inferences between variables, to determine a degree of correlation between two or more variables, or the like. 
     Still referring to  FIG.  6   , machine-learning module  600  may be designed and configured to create a machine-learning model  624  using techniques for development of linear regression models. Linear regression models may include ordinary least squares regression, which aims to minimize the square of the difference between predicted outcomes and actual outcomes according to an appropriate norm for measuring such a difference (e.g. a vector-space distance norm); coefficients of the resulting linear equation may be modified to improve minimization. Linear regression models may include ridge regression methods, where the function to be minimized includes the least-squares function plus term multiplying the square of each coefficient by a scalar amount to penalize large coefficients. Linear regression models may include least absolute shrinkage and selection operator (LASSO) models, in which ridge regression is combined with multiplying the least-squares term by a factor of 1 divided by double the number of samples. Linear regression models may include a multi-task lasso model wherein the norm applied in the least-squares term of the lasso model is the Frobenius norm amounting to the square root of the sum of squares of all terms. Linear regression models may include the elastic net model, a multi-task elastic net model, a least angle regression model, a LARS lasso model, an orthogonal matching pursuit model, a Bayesian regression model, a logistic regression model, a stochastic gradient descent model, a perceptron model, a passive aggressive algorithm, a robustness regression model, a Huber regression model, or any other suitable model that may occur to persons skilled in the art upon reviewing the entirety of this disclosure. Linear regression models may be generalized in an embodiment to polynomial regression models, whereby a polynomial equation (e.g. a quadratic, cubic or higher-order equation) providing a best predicted output/actual output fit is sought; similar methods to those described above may be applied to minimize error functions, as will be apparent to persons skilled in the art upon reviewing the entirety of this disclosure. 
     Continuing to refer to  FIG.  6   , machine-learning algorithms may include, without limitation, linear discriminant analysis. Machine-learning algorithm may include quadratic discriminate analysis. Machine-learning algorithms may include kernel ridge regression. Machine-learning algorithms may include support vector machines, including without limitation support vector classification-based regression processes. Machine-learning algorithms may include stochastic gradient descent algorithms, including classification and regression algorithms based on stochastic gradient descent. Machine-learning algorithms may include nearest neighbors algorithms. Machine-learning algorithms may include various forms of latent space regularization such as variational regularization. Machine-learning algorithms may include Gaussian processes such as Gaussian Process Regression. Machine-learning algorithms may include cross-decomposition algorithms, including partial least squares and/or canonical correlation analysis. Machine-learning algorithms may include naive Bayes methods. Machine-learning algorithms may include algorithms based on decision trees, such as decision tree classification or regression algorithms. Machine-learning algorithms may include ensemble methods such as bagging meta-estimator, forest of randomized tress, AdaBoost, gradient tree boosting, and/or voting classifier methods. Machine-learning algorithms may include neural net algorithms, including convolutional neural net processes. 
     Referring now to  FIG.  7   , method of battery ventilation  700  is presented. At step  705 , method  700  includes providing a plurality of vents to a plurality of battery cells. At step  710 , the method  700  includes sensing, via a sensor in electronic communication with a plurality of battery cells, battery cell data. At step  715 , the method  700  includes determining, via a fligh controller of an electric aircraft, a vent arrangement. At step  720 , the method  700  includes adjusting at least a vent of a plurality of vents as a function of a vent arrangement. 
     It is to be noted that any one or more of the aspects and embodiments described herein may be conveniently implemented using one or more machines (e.g., one or more computing devices that are utilized as a user computing device for an electronic document, one or more server devices, such as a document server, etc.) programmed according to the teachings of the present specification, as will be apparent to those of ordinary skill in the computer art. Appropriate software coding can readily be prepared by skilled programmers based on the teachings of the present disclosure, as will be apparent to those of ordinary skill in the software art. Aspects and implementations discussed above employing software and/or software modules may also include appropriate hardware for assisting in the implementation of the machine executable instructions of the software and/or software module. 
     Such software may be a computer program product that employs a machine-readable storage medium. A machine-readable storage medium may be any medium that is capable of storing and/or encoding a sequence of instructions for execution by a machine (e.g., a computing device) and that causes the machine to perform any one of the methodologies and/or embodiments described herein. Examples of a machine-readable storage medium include, but are not limited to, a magnetic disk, an optical disc (e.g., CD, CD-R, DVD, DVD-R, etc.), a magneto-optical disk, a read-only memory “ROM” device, a random access memory “RAM” device, a magnetic card, an optical card, a solid-state memory device, an EPROM, an EEPROM, and any combinations thereof. A machine-readable medium, as used herein, is intended to include a single medium as well as a collection of physically separate media, such as, for example, a collection of compact discs or one or more hard disk drives in combination with a computer memory. As used herein, a machine-readable storage medium does not include transitory forms of signal transmission. 
     Such software may also include information (e.g., data) carried as a data signal on a data carrier, such as a carrier wave. For example, machine-executable information may be included as a data-carrying signal embodied in a data carrier in which the signal encodes a sequence of instruction, or portion thereof, for execution by a machine (e.g., a computing device) and any related information (e.g., data structures and data) that causes the machine to perform any one of the methodologies and/or embodiments described herein. 
     Examples of a computing device include, but are not limited to, an electronic book reading device, a computer workstation, a terminal computer, a server computer, a handheld device (e.g., a tablet computer, a smartphone, etc.), a web appliance, a network router, a network switch, a network bridge, any machine capable of executing a sequence of instructions that specify an action to be taken by that machine, and any combinations thereof. In one example, a computing device may include and/or be included in a kiosk. 
       FIG.  8    shows a diagrammatic representation of one embodiment of a computing device in the exemplary form of a computer system  800  within which a set of instructions for causing a control system to perform any one or more of the aspects and/or methodologies of the present disclosure may be executed. It is also contemplated that multiple computing devices may be utilized to implement a specially configured set of instructions for causing one or more of the devices to perform any one or more of the aspects and/or methodologies of the present disclosure. Computer system  800  includes a processor  804  and a memory  808  that communicate with each other, and with other components, via a bus  812 . Bus  812  may include any of several types of bus structures including, but not limited to, a memory bus, a memory controller, a peripheral bus, a local bus, and any combinations thereof, using any of a variety of bus architectures. 
     Processor  804  may include any suitable processor, such as without limitation a processor incorporating logical circuitry for performing arithmetic and logical operations, such as an arithmetic and logic unit (ALU), which may be regulated with a state machine and directed by operational inputs from memory and/or sensors; processor  804  may be organized according to Von Neumann and/or Harvard architecture as a non-limiting example. Processor  804  may include, incorporate, and/or be incorporated in, without limitation, a microcontroller, microprocessor, digital signal processor (DSP), Field Programmable Gate Array (FPGA), Complex Programmable Logic Device (CPLD), Graphical Processing Unit (GPU), general purpose GPU, Tensor Processing Unit (TPU), analog or mixed signal processor, Trusted Platform Module (TPM), a floating point unit (FPU), and/or system on a chip (SoC). 
     Memory  808  may include various components (e.g., machine-readable media) including, but not limited to, a random-access memory component, a read only component, and any combinations thereof. In one example, a basic input/output system  816  (BIOS), including basic routines that help to transfer information between elements within computer system  800 , such as during start-up, may be stored in memory  804 . Memory  804  may also include (e.g., stored on one or more machine-readable media) instructions (e.g., software)  820  embodying any one or more of the aspects and/or methodologies of the present disclosure. In another example, memory  808  may further include any number of program modules including, but not limited to, an operating system, one or more application programs, other program modules, program data, and any combinations thereof. 
     Computer system  800  may also include a storage device  824 . Examples of a storage device (e.g., storage device  824 ) include, but are not limited to, a hard disk drive, a magnetic disk drive, an optical disc drive in combination with an optical medium, a solid-state memory device, and any combinations thereof. Storage device  824  may be connected to bus  812  by an appropriate interface (not shown). Example interfaces include, but are not limited to, SCSI, advanced technology attachment (ATA), serial ATA, universal serial bus (USB), IEEE 1394 (FIREWIRE), and any combinations thereof. In one example, storage device  824  (or one or more components thereof) may be removably interfaced with computer system  800  (e.g., via an external port connector (not shown)). Particularly, storage device  824  and an associated machine-readable medium  828  may provide nonvolatile and/or volatile storage of machine-readable instructions, data structures, program modules, and/or other data for computer system  800 . In one example, software  820  may reside, completely or partially, within machine-readable medium  828 . In another example, software  820  may reside, completely or partially, within processor  804 . 
     Computer system  800  may also include an input device  832 . In one example, a user of computer system  800  may enter commands and/or other information into computer system  800  via input device  832 . Examples of an input device  832  include, but are not limited to, an alpha-numeric input device (e.g., a keyboard), a pointing device, a joystick, a gamepad, an audio input device (e.g., a microphone, a voice response system, etc.), a cursor control device (e.g., a mouse), a touchpad, an optical scanner, a video capture device (e.g., a still camera, a video camera), a touchscreen, and any combinations thereof. Input device  832  may be interfaced to bus  812  via any of a variety of interfaces (not shown) including, but not limited to, a serial interface, a parallel interface, a game port, a USB interface, a FIREWIRE interface, a direct interface to bus  812 , and any combinations thereof. Input device  832  may include a touch screen interface that may be a part of or separate from display  836 , discussed further below. Input device  832  may be utilized as a user selection device for selecting one or more graphical representations in a graphical interface as described above. 
     A user may also input commands and/or other information to computer system  800  via storage device  824  (e.g., a removable disk drive, a flash drive, etc.) and/or network interface device  840 . A network interface device, such as network interface device  840 , may be utilized for connecting computer system  800  to one or more of a variety of networks, such as network  844 , and one or more remote devices  848  connected thereto. Examples of a network interface device include, but are not limited to, a network interface card (e.g., a mobile network interface card, a LAN card), a modem, and any combination thereof. Examples of a network include, but are not limited to, a wide area network (e.g., the Internet, an enterprise network), a local area network (e.g., a network associated with an office, a building, a campus or other relatively small geographic space), a telephone network, a data network associated with a telephone/voice provider (e.g., a mobile communications provider data and/or voice network), a direct connection between two computing devices, and any combinations thereof. A network, such as network  844 , may employ a wired and/or a wireless mode of communication. In general, any network topology may be used. Information (e.g., data, software  820 , etc.) may be communicated to and/or from computer system  800  via network interface device  840 . 
     Computer system  800  may further include a video display adapter  852  for communicating a displayable image to a display device, such as display device  836 . Examples of a display device include, but are not limited to, a liquid crystal display (LCD), a cathode ray tube (CRT), a plasma display, a light emitting diode (LED) display, and any combinations thereof. Display adapter  852  and display device  836  may be utilized in combination with processor  804  to provide graphical representations of aspects of the present disclosure. In addition to a display device, computer system  800  may include one or more other peripheral output devices including, but not limited to, an audio speaker, a printer, and any combinations thereof. Such peripheral output devices may be connected to bus  812  via a peripheral interface  856 . Examples of a peripheral interface include, but are not limited to, a serial port, a USB connection, a FIREWIRE connection, a parallel connection, and any combinations thereof 
     The foregoing has been a detailed description of illustrative embodiments of the invention. Various modifications and additions can be made without departing from the spirit and scope of this invention. Features of each of the various embodiments described above may be combined with features of other described embodiments as appropriate in order to provide a multiplicity of feature combinations in associated new embodiments. Furthermore, while the foregoing describes a number of separate embodiments, what has been described herein is merely illustrative of the application of the principles of the present invention. Additionally, although particular methods herein may be illustrated and/or described as being performed in a specific order, the ordering is highly variable within ordinary skill to achieve methods, systems, and software according to the present disclosure. Accordingly, this description is meant to be taken only by way of example, and not to otherwise limit the scope of this invention. 
     Exemplary embodiments have been disclosed above and illustrated in the accompanying drawings. It will be understood by those skilled in the art that various changes, omissions and additions may be made to that which is specifically disclosed herein without departing from the spirit and scope of the present invention.