PATENT CLAIM ANALYSIS

Application Number: 15747439
Application Type: Utility
Filing Date: 2018-06
Publication Date: 2018-10
Patent Classification: ["701", "003000"]

Abstract:
A method and system for designing a cooperatively-driven aircraft system. A cooperatively-driven aircraft system comprises an aircraft, a movable ground monitor station or a fixed ground monitor station, a data link of a composite data chain, and a relay communication device. A flight management system is disposed inside the aircraft. The aircraft is connected to the movable ground monitor station or the fixed ground monitor station by means of the radio data link of the composite data chain. Telemetering data information about the flight management system is issued to the movable ground monitor station or the fixed ground monitor station by means of the composite data chain. A manned aircraft technology and an unmanned aerial vehicle system technology are combined, cooperative air and ground driving is constructed, and a new technology aircraft system integrating easy flight and safe flight is provided.

Claim (Index 1):
A method for designing a cooperatively-driven aircraft system, wherein: apparatuses of an aircraft and a ground which monitor and control a flight, together form the cooperatively-driven aircraft system which has complete information and control functions between air and ground; the whole cooperatively-driven aircraft system is divided into three parts: the aircraft, a ground monitor and control system and a data link, the aircraft is configured with a telex manipulation system for a pilot, the pilot uses the telex manipulation system to fly the aircraft, the telex manipulation system has a flight management system as a center, the flight management system is responsible for integrating a telex manipulator, a parameter sensor and a control execution system, provides different control modes of performing a flight for the pilot, and achieves an automatic flight independent of the pilot's sense; the flight management system is a flight task management computer system, achieves a complete function of providing automatic flight control for the aircraft, a flight management computer of the flight management system is also used for the telex manipulation system, achieves a conversion channel between a manual mode and an automatic mode; the ground monitor and control system, is a working environment in which a ground monitor personnel perform monitoring and control of a flight of the aircraft by the data link and corresponding apparatuses; the data link connects the aircraft with a ground monitor station, the data link is a radio link which provides a control instruction or a data information linkage between the air and the ground; the cooperatively-driven aircraft system formed by the aircraft and the ground monitor station together provides different control levels and control modes of performing the flight for an on-board pilot, including the manual mode, a semi-automatic mode and an automatic mode on-board, the ground monitor personnel of the ground monitor station are able to not depend on the on-board pilot, and perform a selectable flight control mode, comprising the manual mode, the semi-automatic mode and the automatic mode, in the flight management system, a data chain connection with the ground monitor station is constructed, accepted or installed data and instruction is processed and executed, the control levels are introduced to provide control laws for the flight management system to control a combination control object of the flight management three convertible control modes, comprising manual control, semi-automatic control and automatic control, are set for the flight management system, so that different driving methods are provided for the pilot when the manual mode is selected for the flight management system, the flight management system becomes the telex manipulation system, and when the semi-automatic mode and the automatic mode are selected, the flight management system becomes a task management system;\n all of the three control modes achieve a control of the combination control object by means of the flight management system; one implementation method for achieving the control of the combination control object by means of the flight management system is, the ground monitor personnel predetermine the control level for the flight management system, the on-board pilot does not change the control level, but selects the control mode, so that in accordance with control data given by the pilot and sensor subsystem data information, the flight management system cooperates to implement and achieve a corresponding control process on a connected combination control object according to a control law given by the control level and a control function thereof; an use of the telex manipulator is a method of the manual mode; an allowed amount of deviation is limited by a flight range; when the deviation reaches a limit and is maintained, the deviated airline will go in a same direction and at a same altitude and at an equal distance, relative to a predetermined airline; design a correction adjustment and control to correct a case where the aircraft deviates from the predetermined airline in the automatic flight by use of a manipulation method of manually manipulating the telex manipulator or a control key, one manipulation generates one correction instruction corresponding to one adjustment quantity of a heading, and according to specific pneumatic characteristics of the aircraft as well as pulse duration time of the correction instruction, a heading correction amount generated by one correction instruction is determined; one key-press or a re-manipulation of the telex manipulator after the telex manipulator returns to the middle generates a new correction instruction, the heading correction amount accumulated for consecutive several times achieves a large change in the heading, and a correction of the heading achieves a correction of an airline deviation; a range of the heading correction amount allowed by the accumulation is set.

Metadata:
- Claim Count in Document: 16.0
- Percentile: 94.0
- Lexical Diversity: 2.57627
- Patent Class: 701.0
- Transitional Phrase Type: open
- Component Type: 1
- Foreign Priority: True
- Related Applications: ['13694746', '14121622', '13998833', '13420664', '12246681']

Analysis Scores:
- 35 USC 101 Eligibility (BERT): 0.4671795121538931
- 35 USC 102 Novelty (BERT): 0.4881141719022042
- Combined Prediction Score: 0.4692729781287242
- Mean Citation Score: 229.569678
- Max Citation Score: 230.38179
- Similarity Product: 164.17736721498008

Labels:
- Claim Label 101: 1
- Claim Label 102: 1
- Claim Label 103: 1
- Claim Label 112: 0
- Combined Label: 1
- Label 101 Adjusted: 1

Dataset: test