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Control allocation and management of redundant control effectors based on bases sequenced optimal method 被引量:6

Control allocation and management of redundant control effectors based on bases sequenced optimal method
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摘要 For an advanced aircraft, the amount of its effectors is much more than that for a traditional one, the functions of effectors are more complex and the coupling between each other is more severe. Based on the current control allocation research, this paper puts forward the concept and framework of the control allocation and management system for aircrafts with redundancy con-trol effectors. A new optimal control allocation method, bases sequenced optimal (BSO) method, is then presented. By analyz-ing the physical meaning of the allocation process of BSO method, four types of management strategies are adopted by the system, which act on the control allocation process under different flight conditions, mission requirements and effectors work-ing conditions. Simulation results show that functions of the control allocation system are extended and the system adaptability to flight status, mission requirements and effector failure conditions is improved. For an advanced aircraft, the amount of its effectors is much more than that for a traditional one, the functions of effectors are more complex and the coupling between each other is more severe. Based on the current control allocation research, this paper puts forward the concept and framework of the control allocation and management system for aircrafts with redundancy con-trol effectors. A new optimal control allocation method, bases sequenced optimal (BSO) method, is then presented. By analyz-ing the physical meaning of the allocation process of BSO method, four types of management strategies are adopted by the system, which act on the control allocation process under different flight conditions, mission requirements and effectors work-ing conditions. Simulation results show that functions of the control allocation system are extended and the system adaptability to flight status, mission requirements and effector failure conditions is improved.
出处 《Science China(Technological Sciences)》 SCIE EI CAS 2010年第2期577-583,共7页 中国科学(技术科学英文版)
基金 supported by the National Natural Science Foundation of China (Grant No. 60804007) the Aviation Science Funds of China (Grant No. 20080751018)
关键词 aircraft with multiple CONTROL EFFECTORS flight CONTROL MANAGEMENT aircraft with multiple control effectors flight control management
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参考文献8

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二级参考文献9

  • 1柳嘉润,申功璋.基于逆动力学和在线参数辨识的飞机姿态控制[J].北京航空航天大学学报,2005,31(2):111-115. 被引量:9
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