Fault-tolerant anti-interference control method for multisource interference system

A technology of interference system and control method, applied in the direction of adaptive control, general control system, control/regulation system, etc., can solve the problem of ignoring information interference information of modelable interference, not making full use of system resources, increasing system conservatism, etc. question

A technology of interference system and control method, applied in the direction of adaptive control, general control system, control/regulation system, etc., can solve the problem of ignoring information interference information of modelable interference, not making full use of system resources, increasing system conservatism, etc. question

CN102749852AActive Publication Date: 2012-10-24BEIHANG UNIV

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  • Fault-tolerant anti-interference control method for multisource interference system
  • Fault-tolerant anti-interference control method for multisource interference system
  • Fault-tolerant anti-interference control method for multisource interference system

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Embodiment Construction

[0047] Such as figure 1 As shown, the specific implementation steps of the present invention are as follows (the following takes the satellite attitude determination and control system as an example to illustrate the specific implementation of the method):

[0048] 1. Build a dynamic model with multi-source interference system and write it as a state space expression

[0049] When the Euler angle between the micro-nano-satellite body coordinate system and the orbital coordinate system is small, the following linearized attitude dynamics and kinematics model of the satellite can be obtained:

[0050] J 1 φ · · - n ( J 1 - ...

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Abstract

The invention relates to a fault-tolerant anti-interference control method for a multisource interference system. Aiming at the multisource interference system containing time-varying faults, modeling interference and non-modeling random interference, a fault-tolerant anti-interference controller is designed. The fault-tolerant anti-interference control method comprises the following steps of: firstly, designing a fault diagnosis observer to estimate and counteract the time-varying faults in the system; secondly, designing an interference observer to estimate and counteract the modeling interference in the multisource interference system; thirdly, designing a robust H infinity state feedback controller to inhibit the non-modeling random interference, fault estimation errors and interference estimation errors in the multisource interference system; and finally, designing the fault-tolerant anti-interference controller based on the fault diagnosis observer, the interference observer and the robust H infinity state feedback controller. The method has the advantages of high anti-interference performance, significant fault-tolerant performance, high working reliability and the like and can be used for altitude control subsystems in the fields of aviation and aerospace.

Description

technical field [0001] The invention relates to a fault-tolerant and anti-jamming control method, in particular to a fault-tolerant and anti-jamming control method for a multi-source jamming system, which can be used for fault diagnosis and fault-tolerant anti-jamming control of a multi-source jamming system, such as satellites, missiles and aircraft, etc. Attitude control subsystem for aerospace systems. Background technique [0002] In recent years, with the development of aerospace technology, the structure and mission requirements of aircraft have become increasingly complex, and the requirements for control accuracy and stability have become higher and higher, resulting in an increasing probability of aircraft failure. For example, some scholars have conducted statistics and analysis on 764 spacecraft successfully launched at home and abroad during 1990-2001, and found that 121 of them had malfunctioned, accounting for 15.8% of the total number of spacecraft. The relia...

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Application Information

Patent Timeline
24 Oct 2012
Publication
CN102749852A
IPC
G05B13/04
Inventors
郭雷; 乔建忠