Control of prime mover in hvac distribution system

Abstract: A controller controls a prime mover (source component) in a heating, ventilation and air-conditioning (HVAC) distribution system. The controller determines a static pressure setpoint for the source component by first determining the pressure loss of each branch throughout the system. The controller then determines the pressure loss contributed by local components located within each branch of the system. The maximum of the branch pressure losses and the maximum of the component pressure losses are summed to provide the static pressure setpoint for the source component. The method provides improved control of the prime mover independent of the configuration of the system, which allows for easy and cost-effective implementation of the control method.

Description: FIELD OF THE INVENTION This invention is generally related to control systems in heating, ventilation, and air-conditioning (HVAC) fluid distribution systems, and more particularly to controlling a prime fluid mover utilized in a HVAC fluid distribution systems. BACKGROUND OF THE INVENTION Fluid distribution systems are well known in the art. One example of a fluid distribution system is the system associated with heating, ventilating and air-conditioning (HVAC) distribution systems. HVAC distribution systems see widespread use in commercial applications, i.e., residential housing, apartment buildings, office buildings, etc. However, HVAC distribution systems also see widespread use in laboratory-type settings. In this implementation, the HVAC distribution system is primarily intended for clean-room use, exhaust of potentially noxious fumes, etc. In a majority of HVAC distribution system implementations, the primary goal is to produce and distribute thermal energy in order to offset the cooling and heating needs of a particular installation. For purposes of analysis, the distribution system can be divided into two subsystems; global and local subsystems. The global subsystem consists of a prime mover (i.e., a source) which might be a fan in an air distribution system or a pump in a water distribution system. Also included in the global subsystem is the duct-work required to connect the global subsystem to the local subsystem. The local subsystem primarily consists of dampers, valves or fume hoods. Current control practice, in both commercial and laboratory HVAC distribution systems, separates the global subsystem from the local subsystem and accordingly treats the individual subsystems independent of one another. The result of this separation is (1) poor controllability, (2) energy waste throughout the system, and (3) costly commissioning (installation and maintenance) processing. The current state-of-the art control strategy for heating and cooling needs is based on varying the volume of air flow as the space thermal load changes. Thus, variable air volume (VAV) systems have become very popular for HVAC distribution systems. The underlying principle of the VAV system is to reduce the cost as the thermal load diminishes. Both the cost of moving the air, i.e. fan energy, and the thermal energy cost to condition the air will reduce with the decrease in volume of air. Since the modulation of the rate of flow of air is necessary, the air distribution fan is equipped with some means of varying the volume of air the fan delivers. This is typically done by varying the speed of the fan. FIG. 1 generally depicts a prior art HVAC distribution system. As depicted in FIG. 1, a fan controller 103 controls the variable air volume by controlling the speed of a fan 106 so that a constant static pressure at an arbitrary duct location (for example, the location 114) is maintained. A damper 118 is controlled by a damper controller 124. The static pressure at the location 114 fluctuates as the flow requirement of the damper 118 varies. However, the fan controller 103 ignores the requirement of static pressure in the entire system so that the flow requirement of the damper 118 can be satisfied. In this scenario, the fan controller 103 attempts to maintain an arbitrarily selected pressure setpoint, which is often set based on a maximum operating design condition. During normal operating conditions, however, the system static pressure requirement is considerably lower than the design condition. This results in a considerable amount of energy waste since the fan continuously operates to satisfy the maximum static pressure setpoint. If, on the other hand, the setpoint is much lower than the system requirement, the system is incapable of satisfying the flow requirements, which results in an ineffective system. In addition, no scientific methods exist to determine the best (optimum) position of the static pressure sensor 112 within the duct 115. In other words, the positioning of the static pressure sensor 112 is more of an art than a science. Furthermore, the tuning of the VAV fan control can be time consuming and costly if the selected pressure setpoint and the position of the static pressure sensor 112 are chosen incorrectly. Another problem associated with the implementation of FIG. 1 is the fixed setpoint for static pressure sensor 112. As VAV boxes 109, 118 are opened and closed, the pressure throughout the system will decrease/increase accordingly. By fixing the setpoint while the pressure fluctuates, energy is wasted because the static pressure is not reduced when VAV boxes 109, 118 do not demand much flow. For the sake of simplicity, if an air system can be assumed to be a closed loop, then the distribution system can be modelled as a parallel electrical circuit. Each branch of the circuit can be represented by a VAV box supplying air to a zone and associated branch ducts/fittings. Typically, in a VAV system the static pressure sensor (like sensor 112) is located in the farthest (or 2/3 downstream in the air duct) branch. Placement at this location assumes the pressure in this branch will be the maximum considering the length of ducts connecting this branch and the fan. In reality, however, the maximum branch pressure loss may be dictated by another branch. For example, if a branch closer to the fan has high pressure loss components, the pressure of the fan P f , will be less than what is required. As a consequence, the branch near the fan will not receive the required air flows. One technique of VAV fan control is based on measuring branch flows and modulating the fan speed to achieve the desired flow Q f exiting the fan. This technique is described by Warren, M., et al., "Integrating VAV Zone Requirements with Supply Fan Operation," ASHRAE Journal, April 1993 and Hartman, T.B., "TRAV - A New Concept," Heating/Piping/Air Conditioning, July 1989. The shortcoming of this approach is that the fan energy output is based on two variables, static pressure and flow. The use of a measured flow as a process variable requires a separate feedback loop. In this case, the fan controller will search for the correct static pressure such that all the branch flow requirements are satisfied. However, the feedback loop may have severe limitations in measuring and exchanging the flow information over the network. Thus, while the response is slow, controllability is likewise affected since the fan controller will continually search for the correct static pressure to generate. Another technique of VAV fan control is to measure the damper position in each branch, and modulate the fan speed until one of the dampers remains almost 100% open. This technique is described by Hartman, T.B., "Direct Digital Controls for HVAC Systems," McGraw-Hill, Inc., 1993. This technique assumes that when at least one damper is nearly 100% open, the minimum limit of the fan static pressure is achieved. This strategy reduces fan energy cost, but may not reach the optimal solution since damper position cannot sufficiently determine the fan control point. Furthermore, the communication problem of data flow and additional cost of positioning sensors remain an issue. Okada, T., et al., "Research and Development of Home Use VAV Air-Conditioning System," ASHRAE Transactions, V.98, Pt. 2, 1992 describe a method of calculating branch resistance for a residential HVAC distribution system by opening one damper at a time. This method, however, is impractical in non-residential buildings due to the presence of large numbers of VAV boxes in such applications. A similar method and system using a pressure differential detector and an air volume detector located at a single location is known from GB-A-2 238 885. Goswami, D., "VAV Fan Static Pressure Control with DDC," Heating/Piping/Air Conditioning, December 1986 describes a method of on-line determination of fan static pressure. This method assumes that control software is able to calculate the system pressure loss in real-time for a given system flow requirement. The method is costly, however, since the control software must have detailed duct information, system layout and pressure loss data to compute the fan static pressure requirement. Additionally, as the distribution system undergoes changes, the data base must be updated making implementation of this approach even more costly. Finally, it may be impossible to develop such data in certain retrofit situations due to non-accessibility to the duct system. Thus, a need exists for a control system which, when implemented in a HVAC distribution system, efficiently controls a prime mover without the energy waste and cost inherent in the prior art. SUMMARY OF THE INVENTION It is therefore an object of the present invention to provide an improved method of controlling a prime mover implemented in a heating, ventilation and air-conditioning (HVAC) distribution system. Another object is to provide an improved method of controlling a prime mover which is based on pressure losses of branches and pressure losses across components implemented within the branches. A related object is to provide an improved method of controlling a prime mover which controls the prime mover based on a combination of the branch and the component pressure losses. Another object is to provide an improved method of controlling a prime mover by determining a static pressure setpoint requirement, measured at the output of the prime mover, with the pressure loss due to each branch and each component regardless of, inter alia, the duct information, system layout/configuration or pressure loss data determined a priori. A related object is to provide an improved method of controlling a prime mover that can be easily and cost-effectively implemented in new structures and retro-fitted into existing structures. The above and further objects which will become apparent hereinafter are achieved by a method of controlling a prime mover in a heating, ventilation and air-conditioning distribution system, as defined in the appended claims. These and other objects will become apparent upon reading the following detailed description of the preferred embodiment of the present invention, while referring to the attached drawings. BRIEF DESCRIPTION OF THE DRAWINGS FIG. 1 generally depicts, in block diagram form, a prior art control system implemented in a HVAC system. FIG. 2 depicts, in block diagram form, a HVAC system under control in accordance with the invention. FIG. 3 generally depicts the global control strategy implemented in the local controller and source controller of FIG. 2 in accordance with the invention. FIG. 4 generally depicts, in block diagram form, the control process of FIG. 3 implemented in a local controller for controlling a local component in accordance with the invention. FIG. 5 generally depicts, in block diagram form, the control process of FIG. 3 implemented in a source controller for controlling a source component in accordance with the invention. DETAILED DESCRIPTION OF A PREFERRED EMBODIMENT Generally stated, a prime mover in a heating, ventilation and air-conditioning (HVAC) distribution system, which has components located within branches of the HVAC distribution system, is controlled by first determining a first plurality of pressure losses for a corresponding plurality of branches of the HVAC distribution system. Then, a second plurality of pressure losses for a corresponding plurality of components located in the plurality of branches of the HVAC distribution system. Finally, the prime mover is controlled based on a relationship between the first plurality of pressure losses and the second plurality of pressure losses. In the preferred embodiment, the components of the HVAC fluid distribution system are a fan and a damper. The identified characteristics of the fan are a pressure setpoint ( P fsp ) and a flow setpoint ( Q fsp ) of air at the output of the fan, and a fan control signal ( Y l / f ). The identified characteristics of the damper are an authority ( A^ ) and a percentage of flow (% FullFlow ) of the damper, and a damper control signal ( Y l / d ). In an alternate embodiment, the authority ( Â ) may be replaced by a static pressure at the inlet of the damper ( P il ) for small distribution systems since the damper authority Â may not vary a significantly. Also in the preferred embodiment, the controller includes a feedforward means for generating a feedforward control signal based on the identified characteristics of the component and calculated system variables and a feedback means for generating a feedback control signal based on measured system variables. The controller then controls the component based on a combination of the feedforward control signal and the feedback signal. A control system is implemented in a fluid distribution system in accordance with the present invention as shown in FIG. 2. As stated above, the preferred embodiment fluid distribution system is a HVAC system. However, as one of ordinary skill in the art will appreciate, the control system described hereinafter may be beneficially employed in any fluid distribution system with qualities similar to HVAC systems. The block diagram of FIG. 2 depicts a HVAC system primarily intended for use in commercial settings, but may be easily modified to perfo in laboratory settings. All fluid flow is measured in units of cubic meter per second (cubic feet per minute (cfm)), while all pressures are measured in units of Pa (inches of water gauge (w.g.)). The embodiment of FIG. 2 relates to an air distribution system in a commercial setting, but as one of ordinary skill in the art will appreciate, the apparatus may be beneficially implemented in laboratory buildings as well. In commercial buildings, the goal is to provide thermal comfort while lowering energy cost, while in laboratory buildings a third goal of safety is added. Continuing, the source component 203 is implemented as a fan 203, while the local component 221 is implemented as a damper 221. As one of ordinary skill in the art will again appreciate, the source component 203 may be implemented as any prime mover (pump, etc.) depending on the system of choice, while the local component 221 may be implemented as any controllable variable air flow device (fume hood, supply boxes, general exhaust boxes, etc.). In the embodiment depicted in FIG. 2, a static pressure sensor 209 is not arbitrarily located, but instead is located at the output of the fan 203. This is done so that the fan static pressure P f will be utilized in the same manner by the source controller 236, no matter what the configuration of the system. In other words, the fan static pressure P f can be correlated to a particular system independent of the configuration of the system. As also depicted in the embodiment of FIG. 2, the setpoint of the static pressure sensor 209 is allowed to vary to accommodate varying pressure in the main duct 215 due to the opening/closing of the damper 221. Allowing the setpoint of the static pressure sensor 209 (and consequently static pressure P f and flow Q f at the output of the fan 203) to vary is significant since the energy (in horsepower) of the fan 203 is proportional to the product of the static pressure P f and the flow Q . Thus, for example, a 50% savings in static pressure P f translates to a 50% energy savings in operation of the fan 203. Because of the new relationship between the static pressure P f and the flow Q f at the output of the fan 203 and the static pressure P il and the flow Q il related to the damper 221, a data exchange between the local controller 224 and the source controller 236 is necessary. Data exchange between the source controller 236 and the local controller 224 occurs via the lines 230-233 as depicted in FIG. 2. The line 230 transfers a damper flow setpoint Q ilsp from the local controller 224 to the source controller 236, while the line 231 transfers the static pressure P il and the flow Q il measured at the inlet of the damper 221. The transferred static pressure P il and the flow Q il are measured by the static pressure sensor 219 and the flow sensor 218 respectively, each being located at the inlet of the damper 221. The line 231 exchanges data periodically for updating the identification of the system flow versus pressure loss relationship. As one of ordinary skill in the art will appreciate, many well known techniques exist to measure the static pressures P f and P il and the flows Q f and Q il at the locations depicted in FIG. 2. One technique is to utilize solenoids configured to aid in the measurement. Important to note is that it may be feasible to calculate the pressure loss across the damper 221 by having only the inlet static pressure P il . In that case, only a single solenoid would be required. The use of solenoids to measure static pressure may be implemented in commercial buildings because of the differential pressure range compatibility with a known flow sensor. For laboratory applications, however, an additional static pressure sensor would be required instead of a solenoid due to the small range of differential pressure required to be measured. The static pressure sensor will be sufficient for laboratory applications since the static pressure measurement is utilized for characterizing the damper 221, and not for control of the damper 221. Input from only a single local controller 224 is depicted in FIG. 2 for simplicity. In a practical implementation, the source controller 236 would receive inputs from a plurality of networked local controllers (not shown), each of the plurality of local controllers controlling their own local component. The networked local controllers would then be coupled to the source controller 236. Consequently, when the source controller 236 receives inputs from all of the local controllers in a particular implementation, the source controller 236 determines an air flow setpoint Q fsp requirement and then determines a fan pressure setpoint P fsp requirement from the system flow versus pressure loss relationship. Also depicted in FIG. 2 is a data exchange from the source controller 236 to the local controller 224 via the lines 232 and 233. The line 232 transfers the pressure setpoint P fsp requirement of the fan 203 as determined by the source controller 236, while the line 233 transfers the measured static pressure P f and the flow Q f at the output of the fan 203. The line 233 exchanges data periodically for updating the identification of the damper 221. Based on the pressure setpoint P fsp requirement, the local controller 224 calculates the static pressure P il . Once the static pressure P il and the flow setpoint Q ilsp of the damper 221 are known, the local controller 224 generates the required control signal 227. Under control from the control signal 227, the damper 221 will either open or close depending on the required control. A global control strategy implemented in the local controller 224 and the source controller 236 of FIG. 2 is shown in FIG. 3 in accordance with the invention. As depicted in FIG. 3, the controllers 224 and 236 are divided into separate processes, an identification process 306 and a control process 303. Separation of the identification process 306 from the control process 303 allows the identification process 306 to be implemented periodically, adaptively, in real-time, while allowing the control process 303 to be implemented continuously. Separating the two processes results in the advantage that the performance of the control process 303 is not sacrificed by allowing the identification process 306 to operate adaptively, in real-time. The identification process 306 identifies certain characteristics of either the damper 221 or the fan 203. These identified characteristics are output to the control process 303 via a line 307. The control process 303 accepts the identified characteristics, along with other signals shown in FIG. 3, and outputs a control signal (via the line 227 to the damper 221 or via the line 206 to the fan 203) so as to provide global control of the HVAC system 309 in accordance with the invention. In the preferred embodiment, the identification process 306 utilizes a look-up table (not shown) to store characteristics of either the damper 221 or the fan 203. For the damper 221, these characteristics are the ratio of the pressure drop across the damper 221 to the branch pressure drop when the damper 221 is fully open (authority, Â ), the percentage of flow through the damper 221 normalized to the maximum flow through the damper 221 (% FullFlow ), and the damper control signal ( Y l / d ). The authority Â can be replaced by inlet static pressure P il in small systems as explained above. For the fan 203, these characteristics are the pressure setpoint ( P fsp ), the summation of the flow setpoints from each local controller ( Q fsp ), and the fan control signal ( Y l / f ). These identified characteristics are output from the identification process 306 as identified characteristics via line 307. Choice of which stored characteristics to identify and output via line 307 is dependent on the values of the measured system variables and the control signal input into the identification process 306. The control process 303 implemented in the local controller 224 for controlling a local component 221 in accordance with the invention is depicted in FIG. 4. As depicted in FIG. 4, the process implemented within the control process 303 is divided into a feedforward process 403 and a feedback process 420. In prior art controllers for HVAC systems (for example the controller 124 of FIG. 1), only the feedback process 420 was implemented. In those systems, the feedback process 420 would operate as a proportional-integral-derivative (PID) control loop, which is a well known technique in the art. As such, only measured values (for the example of the local controller 224) of Q il were utilized. However, due to the noise inherent in the measured system variable Q il , the accuracy of the generated control signal suffered. As depicted in FIG. 4, the feedback process 420 accepts as input a calculated Q ilsp and also a feedforward control signal ( Y^ ) via a line 419. These signals are utilized by the feedback process 420 to generate a control signal 227 with a higher degree of accuracy. The outputs of the feedforward process 403 are calculated signals, which are thus not dependent on any measured values. If the calculated Q ilsp is ideal, it should be equivalent to the measured Q il , thus resulting in zero error exiting the node 423. If zero error enters the blocks 426, 429 and 432, the last utilized control signal will again be output as the feedback control signal 436. If the feedforward control signal Y and on the line 419 is calculated to be the same as the feedback control signal on the line 436, the control signal on the line 227 exiting the node 438 will be the same as in the prior iteration. If the calculated signals provide the majority of control when compared to the measured signals, the effects of noise on the generation of control signal 227 is greatly reduced. In this manner, the feedforward process 403 operates in conjunction with the feedback process 420 to produce a more accurate control signal on the line 227 in accordance with the invention. When implemented in the local controller 224, the feedforward process 403 starts by first receiving the fan static pressure setpoint P fsp on the line 232. This is performed at the block 406 of FIG. 4. The fan static pressure setpoint P fsp is routed to the block 409 where the pressure loss, P lossi , is calculated for each of the i branches connecting the fan outlet and the individual local damper. In the preferred embodiment, the pressure loss P lossi for each of the i branches is determined adaptively, in real-time. To calculate the pressure loss for branch 1, i.e., P lossl , the following steps should be followed. Calculation of the pressure loss P lossl for branch 1 begins by calculating the pressure loss for a first segment of the branch 1, which is from the outlet of the fan 203 to the inlet of the damper 221. The general equation to calculate the pressure loss P loss is given by: P loss = K * Q 2 where P loss = pressure loss, K = friction coefficient, and Q = flow rate. In this example, only the branch 1 pressure loss P lossl is calculated for simplicity. Referring to FIG. 2, the air flow from the fan 203 through the branch 1 can be segmented into smaller paths. The pressures P f , P l , P il , P ol and P xl as shown in FIG. 2 have locations as follows: P f = static pressure @ output of the fan 203, P l = static pressure @ input to branch 1, P il = static pressure @ inlet to the damper 221 within branch 1, P ol = static pressure @ output of the damper 221 within branch 1, and P xl = static pressure @ input to the local area serviced by branch 1. The pressure loss P lossl for branch 1 from the fan 203 through the branch 1 is given by the expression P f - P xl , and can be written as, P f - P xl = ( P f - P il ) + ( P il - P ol ) + ( P ol - P xl ) where P f - P il = ( K fl * Q 2 f ) + ( K l il * Q 2 il ) Equation (3) represents the pressure loss from the outlet of the fan 203 to the inlet of the damper 221. Once the constants K fl , K lil of equation (3) are determined, it is possible to calculate the pressure loss from the outlet of the fan 203 to the inlet of the damper 221 in branch 1. Two subsegments of the first segment need to be considered to determine the friction coefficients K fl and K lxl of equation (3); P f -to- P l and P l -to- P il . Assuming that P f , P il , Q f , and Q il will be measured, K fl and K lxl are the only unknown quantities. By measuring n sets of values of P f , P il , Q f , and Q il , and substituting these sets of values into equation (3) n times, the resulting equations can be solved for the unknown friction coefficients K fl and K lxl by simple regression. As the system goes into operation, more sets of P f , P il , Q f , and Q il can be collected and used to constantly update and refine the values of K fl and K lxl . This step is repeated for each additional branch, recognizing that K fl is known from the prior determination. The next step is to calculate the pressure loss of a second segment, which is from the inlet to the damper 221 to the inlet of the local area serviced by the branch 1. The pressure loss of the second segment can be determined using the expression: P il - P xl = ( Co * Q 2 il ) + ( K olxl * Q 2 il ) The first term of the equation (4) (having Co as a friction coefficient) is the pressure loss across the damper 221, while the second term of the equation (4) (having K olxl as a friction coefficient) is the pressure loss from the output of the damper 221 to the inlet of the local area serviced by the branch 1. The friction coefficient Co has the general nature: Co = m l e -( m 2 * %open ) where m 1 , m 2 and K olxl are constants to be determined. The %open is feedback signal from the damper 221 which indicates the position of the damper 221 by indicating the percentage the damper 221 is open when compared to the damper 221 being fully open (dfo). Substituting the equation (5) into the equation (4) yields: P il - P xl = ( m 1 e -( m 2 * % open ) * Q 2 il ) + ( K olxl * Q 2 il ) When the %open is available, the damper position is adjusted n times (yielding correspondingly different values for %open ) and P il and Q il are measured n times. The pressure P xl is estimated to be 12,405 Pa (0.05 inches per water gauge (w.g.)). With the measured data and the corresponding %open values, the constants m 1 , m 2 and K olxl can be determined through simple regression. The equation (6) can then be utilized to calculate the pressure loss for the second segment. This pressure loss is added to the pressure loss for the first segment to yield the pressure loss P lossl for the branch 1. The equation (6) can also be used if the %open is not available. In this calculation, values of m 1 and m 2 obtained from tables available from ASHRAE are inserted into the equation (6). The damper is fully opened (i.e., %open = 100), and P il and Q il are measured n times. With the damper fully open, the speed of the fan 203 is modulated (n times) and again P il and Q il are measured. The values of m 1 , m 2 , P il and Q il are inserted into the equation (6), which is then solved iteratively to determine the value for the constant K olxl . At this point, the equation (6) can again be utilized to calculate the pressure loss for the second segment. This pressure loss is added to the pressure loss for the first segment to yield the pressure loss P lossl for the branch 1. Important to note is that the above described method of calculating pressure loss P lossi applies for i additional branches connected to the main duct 215. In that situation, the number of duct segments will increase as the distance between the fan 203 and the branch take-off from the main duct 215 increases. The above procedure can be progressively used to calculate the " K " values of each segment of the duct in finding the friction coefficients of flow sensors for each damper utilized in the system. After the pressure loss P lossl for the branch 1 has been calculated, the feedforward process 403 utilizes the calculated P lossl to calculate the inlet static pressure P il at the inlet of the damper 221. This is done in the block 415 by subtracting the calculated pressure loss P lossl from the static pressure set point P fsp received as an input to the block 406. In parallel to the blocks 409 and 415, the feedforward process 403 obtains, in the block 412, the flow setpoint Q ilsp of the damper 221 from a temperature control loop in the controller (not shown). The flow setpoint Q ilsp exiting the block 412 is input into the feedback process 420, and represents the calculated flow setpoint Q ilsp . The flow setpoint Q ilsp exiting the block 412 is also input into the block 418, together with the calculated inlet static pressure P il calculated in the block 415. The block 418 also has as input identified characteristics input on the line 307. The identified characteristics are determined by the identification process 306 of FIG. 3. In the embodiment depicted in FIG. 4, the identified characteristics input on the line 307 are related to the damper 221. The block 418 uses the flow setpoint Q ilsp and the calculated inlet static pressure P il , together with the identified characteristics (stored values of authority Â , %FullFlow, and Y l / d ), to generate the feedforward control signal Y and to be output on the line 419. To effectively calculate the feedforward control signal Y and , a General Regression Neural Network (GRNN) is implemented in the preferred embodiment of the present invention. For a discussion of GRNN, reference is made to A General Regression Neural Network, Donald F. Specht, IEEE Transactions on Neural Networks, vol. 2, no. 6, November 1991, which is specifically incorporated herein by reference. A GRNN is chosen to generate the feedforward control signal Y and 419 for given values of Â and %FullFlow due to its simplicity, robustness and excellent capability in system identification. Unlike conventional neural networks, a GRNN requires little or no training for small data sets while effectively capturing system properties from past history. A GRNN is a one-pass learning algorithm having a highly parallel structure which performs forward path estimates by estimating probability density functions. Even with sparse data in a multi-dimensional measurement space, the algorithm provides smooth transitions from one observed value to another. The algorithmic form can be used for any regression problem in which an assumption of linearity is not justified. If the joint probability density function of X and Y (as an example) are known, then the conditional probability density function and the expected value can be computed. In this case, the joint probability density functions will be estimated from examples using non-parametric estimates. The resulting regression equation can be implemented in a parallel, neural-network-like structure. The structure of data is determined directly from past data, the structure is trained and generalized without feedback. The network also estimates values of X and Y for any new value of X in the short time determined by the propagation time through four layers of the neural network. The GRNN is preferably implemented in an integrated circuit (not shown), thus eliminating the software development process to a large extent. This implementation also eliminates software coding during field installation. In the preferred embodiment, the GRNN is implemented in the block 418. The basic equation for a GRNN is where E [ y\X ] = the conditional mean of y on X, f ( X , y ) = the known joint continuous probability density function y = a scalar random variable, x = a vector random variable, X = a particular measured value of the random variable x. The probability estimate is based on the parzen estimator as described by Specht, supra. A physical interpretation of the probability estimate is that it assigns sample probability of width a for each sample. The probability estimate f and is the sum of those sample probabilities. Substituting the joint probability estimate f and into the conditional mean gives the desired conditional mean of y given on X ( Y and ( X )): where Y and ( X ) = the feedforward control signal Y and as a function of X , D 2 / i = ( X - X i ) T ( X - X i ), X = desired (forward) values of Â and %FullFlow, X i = stored (past) values of Â and %FullFlow, Y ' = stored (past) value Y l / d of the control signal Y and , and σ = width for the same probability. In the block 418, the desired value of the authority Â is first determined. The authority Â can generally be expressed as: Â = ( P il - P ol )| dfo ( P f -P xl )| dfo where dfo signifies that the damper 221 is fully open. From equation (4), the pressure loss across the damper 221 is given by the first term (having Co as a friction coefficient). Consequently, the pressure loss across the damper 221 when the damper 221 is fully open ( P il - P ol )| dfo can be calculated using the expression: ( P il - P ol )| dfo = Co % open = 100 * Q 2 dmax where Q 2 / dmax is the maximum permissible flow through the damper 221. Q dmax can be determined by measuring P il at full flow, and using the equation (6) for %open =100 and the determined values of m 1 , m 2 and K olxl . The constant Co %open =100 can be determined as described above when the %open value is available, or will be known in the case where the %open value is not available by sending the maximum control signal to the damper 221 and insuring that the maximum flow is achieved. The path pressure loss when the damper 221 is fully open ( P f - P xl )| dfo can be calculated once the damper pressure loss at full flow is known and using the flow v. pressure loss relationship generally described in equations (1) and (3): ( P f - P xl )| dfo = ( K fl * Q 2 f ) + ( K l il * Q 2 dmax ) + ( P il - P ol )| dfo + ( K xl * Q 2 dmax ) At this point, equations (10) and (11) can be used to solve for the authority Â . The desired value for the %FullFlow can also be calculated using the expression: % FullFlow = Q ilsp Q dmax * 100 The maximum flow Q dmax is known from above. The flow setpoint Q ilsp is provided to the block 418 from the block 412. Having determined the desired values for the authority Â and the % FullFlow , the GRNN can be used to predict the feedforward control signal Y and ( X ). The stored values of the authority Â , %FullFlow, and Y l / d are received by the block 418 as identified characteristics via the line 307. All values can be inserted into equation (8) to generate the feedforward control signal Y and ( X ), which is output from the block 418 via the line 419. FIG. 5 generally depicts, in block diagram form, the control process 303 of FIG. 3 implemented in the source controller 236 for controlling a source component in accordance with the invention. The functionality of the feedback process 520 is essentially the same as the feedback process 420 of FIG. 4, thus like numerals between the feedback process 520 and the feedback process 420 depict like operations. The feedforward process 503 begins at the block 506 where the flow setpoint Q ilsp 230 is received from each local controller implemented in the HVAC system 309. Again, FIG. 2 only depicts a single branch (branch 1) system, but the feedforward process 503 applies for any and all branches implemented within the HVAC system 309. Continuing, the flow setpoint Q ilsp received from the local controller 224 is sent to the block 509 where the pressure loss P lossi is calculated for each branch (only P lossl for branch l is calculated above). The calculation in the block 509 utilizes the static pressure P il and the flow Q il of the damper 221 received via the line 231 to calculate the pressure loss P lossl as described in relation to the block 409 above. Once the branch pressure loss P lossl is calculated (as well as the pressure loss P lossi for all other branches), the calculated pressure loss values are input into the block 515 where the fan static pressure P fsp is calculated. The fan static pressure P fsp is equal to the sum of the maximum pressure loss of all of the pressure losses P lossi received for each branch and the maximum pressure loss of all of the pressure losses P lossdi incurred by the dampers. The pressure loss P lossdi incurred by a damper is a portion of the pressure loss due to the second segment as shown in equation (4). Important to note is that the damper providing the maximum pressure loss P lossdi need not be associated with the branch having the maximum pressure loss P lossi . As an example, a branch 2 (not shown) may contribute the maximum branch pressure loss ( P loss2 in that case), while the damper 221 of branch 1 may contribute the maximum pressure loss ( P lossdl in that case). These two pressure losses would be added to yield the fan setpoint P fsp . After being calculated, the fan setpoint P fsp is input into the feedback process 520 and represents the calculated fan setpoint P fsP . In parallel with the blocks 509 and 515, the fan flow setpoint Q fsp is calculated in the block 512 by summing all of the flow setpoints Q isp received in the block 506. The fan flow setpoint Q fsp exiting the block 512, together with the fan static pressure P fsp exiting the block 515, is input into the block 518. Also input into the block 518 is the identified characteristics of the fan 203 via the line 307. In the preferred embodiment, the identified characteristics of the fan 203 are stored values of a pressure setpoint ( P fsp ) and a flow setpoint ( Q fsp ) of air at the output of the fan 203, and a fan control signal ( Y l / f ). The block 518 utilizes the calculated fan flow setpoint Q fsp exiting the 512 and the calculated fan static pressure P fsp exiting the block 515, together with the stored values of the pressure setpoint ( P fsp ) and a flow setpoint ( Q fsp ) of air at the output of the fan 203, and a fan control signal ( Y l / f ), to generate the feedforward control signal 519 as required for a fan flow setpoint Q fsp and a fan pressure setpoint P fsp . Again, equation (8) of the GRNN model described above, is utilized where Y and ( X ) = the feedforward control signal Y and as a function of X , D 2 / i = ( X - X i ) T ( X - X i ), X = desired (forward) values of P fsp and Q fsp , X i = stored (past) values of P fsp and Q fsp ; Y' = stored (past) value Y l / f of the control signal Y and , and σ = width for the same probability. Insertion of these values into equation (8) yields the feedforward control signal Y and , which is output from the block 518 via the line 519 . In the preferred embodiment, the local controller 224 is a modified Terminal Equipment Controller (TEC) from the System 600 controller family manufactured by Landis & Gyr Powers. The TEC of the System 600 controller family is commercially available and is extensively documented. The User Reference Manual, Part No. 125-1940 for the TEC of the System 600 controller family is specifically incorporated herein by reference. Also in the preferred embodiment, -the source controller 236 is a modified Modular Building Controller (MBC) from the System 600 controller family. The MBC of the System 600 controller family is commercially available and is extensively documented. The User Reference Manual, Part No. 125-1992 for the MBC of the System 600 controller family is specifically incorporated herein by reference. The modification required to implement the TEC and the MBC of the System 600 controller family is the addition of the identification process 306, the feedforward process 403 or. 503 and the data exchange between the local controller 224 and the source controller 236, each of which has been described herein. While various embodiments of the present inventions have been shown and described, it should be understood that various alternatives can be used. For example, in one alternate embodiment where adequate correlation between the calculated variables and the measured variables exist, the feedback processes 420 and 520 may be completely eliminated. In this embodiment, only the identification process 303 and the feedforward processes 403 or 503 are required to generate the control signal to control the desired component. Various features of the present invention are set forth in the following claims. Where technical features mentioned in any claim are followed by reference signs, those reference signs have been included for the sole purpose of increasing the intelligibility of the claims and accordingly, such reference signs do not have any limiting effect on the scope of each element identified by way of example by such reference signs.

Claims: A method of controlling a prime mover (203) in a heating, ventilation and air-conditioning (HVAC) distribution system, the HVAC distribution system having components (221) which incur a pressure loss, the components (221) located within branches of the HVAC distribution system, the method comprising the steps of: I) determining a first plurality of pressure losses for a corresponding plurality of branches of the HVAC distribution system, the determining of the first plurality of pressure losses comprising for each branch: i) determining the pressure loss for a first segment of the branch; ii) determining the pressure loss for a second segment of the branch, wherein the second segment of each branch is different from the first segment of each branch; and iii) summing the pressure losses for the first and second segments to arrive to the pressure loss for each branch; II) determining a second plurality of pressure losses for a corresponding plurality of components (221) located in the plurality of branches of the HVAC distribution system; and III) controlling the prime mover (203) based on a relationship between the first plurality of pressure losses and the second plurality of pressure losses. The method of claim 1 wherein the component (221) further comprises one of the group of a damper, a fume hood, a supply box, or a general exhaust box. The method of claims 1 or 2 wherein the prime mover (203) further comprises one of the group of a fan or a pump. The method of one or more of claims 1-3 wherein the first segment extends from an output of the prime mover (203) to an inlet of the component (221) located within the particular branch; and the second segment extends from the inlet to the component (221) located within the particular branch to an input of a local area serviced by the particular branch. The method of one or more of claims 1-4 wherein the step of determining a first plurality of pressure losses for a corresponding plurality of branches further comprises the step of determining a pressure loss for each branch utilizing a flow setpoint (Q ilsp ) related to the component (221) located within the particular branch. The method of claim 5 wherein the step of determining a pressure loss for each branch utilizing the flow setpoint (Q ilsp ) related to the component (221) located within the particular branch further comprises the step of receiving the flow setpoint (Q ilsp ) from a controller (224) which controls the component (221) located within the particular branch. The method one or more of claims 1-6 wherein the step of controlling further comprises the step of setting a setpoint requirement (Q fsp , P fsp ) for the prime mover (203). The method of claim 7 wherein the step of setting the setpoint requirement (Q fsp , P fsp ) for the prime mover (203) further comprises the step of setting a static pressure setpoint requirement (P fsp ) for a static pressure at the output of the prime mover (203). The method of claim 8 wherein the step of setting the static pressure setpoint requirement (P fsp ) further comprises the step of setting a static pressure setpoint requirement based on the sum of the maximum pressure loss of the first plurality of pressure losses and the maximum pressure loss of the second plurality of pressure losses.

Inventors: AHMED OSMAN, AHMED, OSMAN
Applicants: LANDIS & STAEFA INC, LANDIS & STAEFA, INC.
Application year: 1995
Main classification: F24F11
IPC codes: F24F11, F24F7, G05D7