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Design method of cooperative driving aircraft system and the system

A design method and aircraft technology, applied in the field of aviation, can solve problems such as inflexible use methods

Active Publication Date: 2015-11-25
陶文英
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The flight control method of UAV is different from the flight control method of manned aircraft. The route generation needs to be pre-established, or temporarily generated quickly, and the method of use is not flexible. It is still necessary to write the program first and then install it into the UAV system.
This is a typical human-machine control process, that is, people write programs to the machine, and then the machine executes the program according to the program, and there is always an obvious time interval

Method used

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  • Design method of cooperative driving aircraft system and the system
  • Design method of cooperative driving aircraft system and the system
  • Design method of cooperative driving aircraft system and the system

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0192] An optional driving method for an on-board pilot and a method for realizing flight control of an aircraft 1 by an on-board flight management system.

[0193] 1. Flight management system such as image 3 As shown, the upper dotted line box in the figure: parameter sensor subsystem; the middle dotted line box: combined control and execution subsystem (control object: attitude, performance, range, level, mode); the lower dotted line box: monitoring / manipulation subsystem ( The cockpit integrated avionics system is also called the electronic flight instrument system EFIS, which includes the CDU. In the manual mode, the flight management system and the CDU exchange data information or control data with the pilot. In the automatic mode, it no longer interacts with the pilot but only provides route data display).

[0194] Flight management system and fly-by-wire connection and combined control load, flight management system and CDU operation interface (other by EFIS):

[019...

Embodiment 2

[0212] A method for realizing the flight control of the aircraft 1 jointly by the ground monitoring station and the monitoring personnel and the pilot on board.

[0213] 1. Control and management of aircraft 1 by the ground monitoring station (control level, three ranges), man-machine interface CDU:

[0214] Before the flight, according to the pilot's driving skill level, the control level is determined and pre-installed on the aircraft or in the option display component as the control law of the flight management system for the control object (as shown in Table 1). Through the composite data link on the ground monitoring station to download data information or upload control information, the monitoring personnel can obtain real-time flight information through its man-machine interface, and monitor and control the flight of the aircraft. In order to save data link bandwidth resources, the flight management system can classify and manage the downloaded data information, and dow...

Embodiment 3

[0224] The sporty type of co-pilot aircraft is mainly used for teaching flight training and sightseeing flight experience. The number is large and representative. It mainly uses single-seater, two-seater, four-seater and less than 19-seater aircraft. Its design methods and products can be used concurrently. It can be expanded to become a business type, especially a private business type co-pilot aircraft. The design method of the sports type is basically the same as that of the cargo type and the industrial and agricultural type co-pilot aircraft. For industrial and agricultural aircraft, the pilot's operation of the flight can play the role of maneuverability and random changes in air operations, and play a role in the taxiing phase of the airport.

[0225] The typical process of flying a sports co-pilot aircraft is as follows:

[0226] 1. Airspace

[0227] For the take-off and landing airports used by the co-piloted aircraft, the flight airspace and waiting airspace are de...

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Abstract

The invention discloses a design method of a cooperative driving aircraft system and the system. Technologies of a manned aircraft and an unmanned aircraft system are combined. Air and ground cooperation driving is constructed. A new technology aircraft system of easy flight and safe flight is provided. Technologies of aerial driving, ground monitoring, air and ground cooperation driving flight, navigation and flight control, data link and navigation monitoring system and the like, and updating and development of a whole industry value chain of a corresponding navigability standard and approval laws and regulations, flight space management laws and regulations, a driver training method, an aircraft design and manufacturing technology, a flight application and business mode and the like are covered. The new aviation technology can be applied to airplanes of commercial transportation, general aviation, military aviation and the like so as to promote development of a new aviation industry. Especially for the airplanes applied to motion of the general aviation, an official business, freight transport and industrial and agricultural usage, an aviation tradition of depending on a professional driver is changed and public flight time in which general public flies a plane is opened.

Description

technical field [0001] The invention relates to an aircraft between a manned aircraft and an unmanned aerial vehicle system, which is integrated into a novel aircraft system, and belongs to the field of aviation technology. Background technique [0002] The current manned aircraft technology is centered on the pilot, and the main performances are: 1. The main pilot or captain is responsible for the flight crew and flight safety when the aircraft takes off the ground; 3. After the aircraft leaves the ground, the ground has no means to enforce flight control. Therefore, the status of the aircraft during flight depends to a large extent on the unilateral judgment and control of the pilot. If the unsafe factors of the pilot are involved, the flight safety of the aircraft will become complicated and difficult to deal with, including flight Factors such as accidental mistakes of the driver, physical health, subjective motivation of driving, etc. Allowing ground monitoring person...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G08G5/00
CPCG05D1/0022G05D1/0061G08G5/0069G08G5/0013G08G5/0026G08G5/006G08G5/0034B64U2201/104G08G5/00G05B19/048H04B7/185B64C39/024
Inventor 陶文英杨绍文
Owner 陶文英
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