| 直升机全包线协调转弯控制律设计及仿真 |
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| 引用本文： | 邢小军,闫建国.直升机全包线协调转弯控制律设计及仿真[J].飞行力学,2011,29(1):42-45. |
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| 作者姓名： | 邢小军 闫建国 |
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| 作者单位： | 西北工业大学自动化学院; |
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| 基金项目： | 国家自然科学基金(60974146) |
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| 摘 要： | 提出了一种应用多目标遗传算法设计直升机全包线协调转弯控制律参数的方法.将侧向过载和倾斜角稳态误差的设计要求转换为不等式约束,并以所有设计包线总体性能Pareto最优作为总目标,以各设计包线性能最优作为子目标,再应用多目标遗传算法自动搜索最优伞包线协调转弯控制律参数.最后,设计了某型直升机协调转弯控制律参数,仿真结果表明...
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| 关 键 词： | 多目标遗传算法 协调转弯 飞行控制律 |
Full-envelop control laws design and its simulation for a helicopter's coordinated turning motion |
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| XING Xiao-jun,YAN Jian-guo.Full-envelop control laws design and its simulation for a helicopter''s coordinated turning motion[J].Flight Dynamics,2011,29(1):42-45. |
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| Authors: | XING Xiao-jun YAN Jian-guo |
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| Institution: | XING Xiao-jun,YAN Jian-guo(College of Automation,Northwestern Polytechnical University,Xi'an 710072,China) |
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| Abstract: | A novel method of flight control laws design for a helicopter's coordinated-turning motion,which was used for a multi-objective genetic algorithm(MOGA),was proposed.Requirements of lateral acceleration and tilt angle's steady-state error were expressed as inequality constraints,obtaining optimal performances in each selected design flight envelop was treated as sub-objectives and that in all selected design flight envelop as overall objectives,and the MOGA was used to solve a multi-objective constrained opt... |
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| Keywords: | MOGA coordinated turning flight control law |
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