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临近空间飞行器新型非相似余度作动/飞控系统容错控制

王军 王巍 张紫君 王效辉 宋志翌 郝晓宇

北京航空航天大学学报2026,Vol.52Issue(8):2756-2768,13.
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北京航空航天大学学报2026,Vol.52Issue(8):2756-2768,13.DOI:10.13700/j.bh.1001-5965.2025.0835

临近空间飞行器新型非相似余度作动/飞控系统容错控制

Fault-tolerant control for near space vehicle with new type dissimilar redundant actuation/flight control system

王军 1王巍 2张紫君 1王效辉 1宋志翌 1郝晓宇3

作者信息

  • 1. 北京自动化控制设备研究所,北京 100074
  • 2. 中国人民解放军 93127部队,北京 100036
  • 3. 航天科工智能机器人有限责任公司,北京 100071
  • 折叠

摘要

Abstract

The paper presents a concomitant model based multi-level fault-tolerant control(FTC)for near space vehicle(NSV)with a new type of dissimilar redundant actuation system(NT-DRAS).The model,with its physical meaning as a virtual system of the actual vehicle,coexists with the real system to perform real-time synchronous simulation and monitoring of the real system's functions and performance status.In order to meet the intelligent decision-making support requirements of the NSV actual system,the concomitant big model consists of a flight control-level main model and actuation-level sub-models that form a hierarchical architecture.In the event that the vehicle's flight attitude-related sensors fail,a hybrid output state can be reconstructed by combining the theoretical output of the flight control-level concomitant main model with the real system usable state.This hybrid output state is then used to solve the state feedback gains using linear quadratic regulator(LQR)technology.Additionally,this study conducts state monitoring and redundancy management for the configured NT-DRAS system at the actuation level,ultimately combining concomitant sub-model based NT-DRAS channel switching measures by flight control-level concomitant main model based LQR control to address complex and progressively deteriorating fault conditions involving actuators and flight control attitude sensors.Finally,numerical simulations are performed on the MATLAB/Simulink platform to verify the effectiveness and progressiveness of the proposed method.

关键词

临近空间飞行器/飞行控制系统/新型非相似余度作动系统/伴生大模型/逐层容错控制

Key words

near space vehicle/flight control system/new type dissimilar redundant actuation system/concomitant model/multi-level fault-tolerant control

分类

航空航天

引用本文复制引用

王军,王巍,张紫君,王效辉,宋志翌,郝晓宇..临近空间飞行器新型非相似余度作动/飞控系统容错控制[J].北京航空航天大学学报,2026,52(8):2756-2768,13.

基金项目

国家自然科学基金(52105049,52307041) National Natural Science Foundation of China(52105049,52307041) (52105049,52307041)

北京航空航天大学学报

1001-5965

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