High-speed aircraft control and fault-tolerant distribution method based on predetermined performance
The invention provides a high-speed aircraft control and fault-tolerant distribution method based on predetermined performance, and relates to the technical field of high-speed aircraft attitude control and fault-tolerant distribution, and the method comprises the steps: constructing a high-speed ai...
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| creator | LIU CHUANKAI LI WENBO SUN JUN BI CHENG DAI HONGHUA LEE NYA-IN YUE XIAOKUI LI XIE HUANG PANXING DING YIBO XU CHENG CHENG JIN PAN XINGHUA SONG CHUANG WEI ZHENYAN |
| description | The invention provides a high-speed aircraft control and fault-tolerant distribution method based on predetermined performance, and relates to the technical field of high-speed aircraft attitude control and fault-tolerant distribution, and the method comprises the steps: constructing a high-speed aircraft attitude model; designing a preset performance function according to the first to-be-designed parameter, and establishing a conversion error system model based on the preset performance function; designing an inner and outer ring controller by adopting a backstepping method aiming at the conversion error system model, designing a self-adaptive updating law for compensating interference, and obtaining a high-speed aircraft attitude control moment instruction through the inner and outer ring controller; and designing a fault-tolerant control distributor according to the attitude control torque instruction and the fault information of the high-speed aircraft, and performing optimization solution on an optimizat |
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| subjects | CONTROL OR REGULATING SYSTEMS IN GENERAL CONTROLLING FUNCTIONAL ELEMENTS OF SUCH SYSTEMS MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS ORELEMENTS PHYSICS REGULATING |
| title | High-speed aircraft control and fault-tolerant distribution method based on predetermined performance |
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