摘要
提出了一种导弹鸭舵/尾舵复合控制方法,在导弹线性化小扰动模型的基础上设计了鸭舵/尾舵复合控制系统,并采用序列二次规划法优化了鸭舵/尾舵复合分配策略。在Matlab/Simulink平台上进行了仿真验证,对导弹控制系统的性能和过载能力进行了分析。仿真结果表明,设计的复合控制方法不仅能够保证控制系统具有良好的动态和稳态特性,还能够确保导弹的高空机动能力,证明了本文算法具有较高的可信性和实用性。
A canard/tail rudder compound control method for missile is presented in this paper.The canard/tail rudder compound control system is designed based on the linearized small disturbance model of missile.The canard/tail rudder compound allocation strategy is proposed and optimized by the sequential quadratic programming method.The performance and overload capability of the control system are analyzed by simulation on Matlab/Simulink.The simulation results show that the compound control method can not only ensure the high dynamic and steady-state performance of the control system,but also ensure the maneuverability of the missile in high altitude,thus proving the algorithm in this paper to be reliable and effective.
作者
黄鲁豫
徐胜利
张明环
HUANG Luyu;XU Shengli;ZHANG Minghuan(College of Astronautics,Northwestern Polytechnical University,Xi’an 710072,Shaanxi,China;Shanghai Electro-Mechanical Engineering Institute,Shanghai 201109,China)
出处
《空天防御》
2019年第3期38-43,共6页
Air & Space Defense
基金
上海航天科技创新基金(SAST2017-010)
关键词
导弹
鸭舵/尾舵
复合控制
序列二次规划
仿真
missile
canard/tail rudder
compound control
sequential quadratic programming(SQP)
simulation
