Volume 37, Number 5, October 2019
|Page(s)||962 - 967|
|Published online||14 January 2020|
A New Compound Control Method for Missile with Canard and Tail Rudders
School of Astronautics, Northwestern Polytechnical University, Xi'an 710072, China
2 Shanghai Academy of Spaceflight Technology, Shanghai 201109, China
3 Shanghai Electro-Mechanical Engineering Institute, Shanghai 201109, China
A new compound control method for missile with canard and tail rudders is presented in this paper. Firstly, the mathematical model of missile with canard/tail rudder is built and linearized using the small disturbance method. Then, the canard/tail rudder compound control system is created; the canard/tail rudder compound allocation strategy is designed based on the sequential quadratic programming method. Finally, the compound control method is verified 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 high maneuverability of the missile in whole airspace with low drag, thus proving the algorithm in this paper to be reliable and effective.
Key words: missile / canard/tail rudder / compound control / sequential quadratic programming / simulation / mathematical model / Matlab/Simulink
关键字 : 导弹 / 鸭舵/尾舵 / 复合控制 / 序列二次规划 / 仿真
© 2019 Journal of Northwestern Polytechnical University. All rights reserved.
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