Flight control law management method and device
A technology of flight control and management method, applied in the field of flight control, can solve the problems of cumbersome configuration process, and achieve the effect of simplifying the configuration process and achieving versatility
Active Publication Date: 2014-12-03
BEIJING AERONAUTIC SCI & TECH RES INST OF COMAC +1
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[0003] In the existing control law management system, due to the different flight control system developers and the different structure systems of the upper computer, the management methods of the flight control computer control laws are also different. The existing control law management systems are usually dedicated The configuration system can only manage the control laws of the dedicated flight control computer
In addition, the existing control law management system needs to reprogram the entire application program to the upper computer for the modification of the control law control parameters. For example, for the modification of a certain control parameter in the control law, the entire application program needs to be reprogrammed. Therefore, the configuration process is more cumbersome
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[0045] The present invention will be further described in detail below in conjunction with the accompanying drawings and embodiments. It should be understood that the specific embodiments described here are only used to explain the present invention, but not to limit the present invention. In addition, it should be noted that, for the convenience of description, only parts related to the present invention are shown in the drawings but not all content.
[0046] figure 1 The flow chart of the flight control law management method provided by the embodiment of the present invention is shown. The method provided by the embodiment of the present invention can be executed by an ordinary personal computer, and the personal computer has at least one of a network interface, a serial port and a USB interface. The personal computer can communicate with the flight control computer through any one of a network interface, a serial port and a USB interface. Such as figure 1 As shown, the p...
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The invention discloses a flight control law management method and device. The method comprises the following steps: establishing a communication connection with a flight control computer based on a unified general protocol; obtaining control parameters configured for the flight control computer; sending the control parameters to the flight control computer through the communication connection and receiving feedback information of the flight control computer; and monitoring running status of control law of the flight control computer according to the feedback information. Through loading the unified general protocol to a personal computer and the flight control computer, and managing the flight control law by adopting a mode of configuring the control parameters, universality of the control law management is achieved; and besides, the configuration process of the control parameters is greatly simplified.
Description
technical field [0001] The invention relates to the technical field of flight control, in particular to a flight control law management method and device. Background technique [0002] The flight control system is one of the key systems on the aircraft, and its main function is to control the aircraft. As the core sub-component of the flight control system, the flight control computer is the main carrier to realize the logic operation, voting and monitoring of the control law. [0003] In the existing control law management system, due to the different flight control system developers and the different structure systems of the upper computer, the management methods of the flight control computer control laws are also different. The existing control law management systems are usually dedicated The configuration system can only manage the control laws of the dedicated flight control computer. In addition, the existing control law management system needs to reprogram the enti...
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IPC IPC(8): G05D1/08
Inventor 康元丽白志强熊斯
Owner BEIJING AERONAUTIC SCI & TECH RES INST OF COMAC