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Canard/Tail Rudder Compound Control Technology Based on Sequential Quadratic Programming |
| HUANG Luyu，XU Shengli，ZHANG Minghuan |
1. College of Astronautics, Northwestern Polytechnical University, Xi’an 710072, Shaanxi， China；
2. Shanghai Electro-Mechanical Engineering Institute, Shanghai 201109, China |
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Abstract 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.
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Received: 30 January 2019
Published: 23 August 2019
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2019, Vol. 2 
