An On-board Rapid Planning Method for Booster Trajectory of Multistage Rocket

Yuxiang Chen, Yongji Wang, Lei Liu, Zhongtao Cheng, Ye Yang
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Abstract

This paper proposes an on-board rapid planning guidance for the boost phase of multistage rockets, based on the Sequential Quadratic Programming (SQP). Firstly, based on the multistage rocket model, Particle Swarm Optimization (PSO) algorithm is used for achieving an initial trajectory by flight trajectory optimization. Secondly, considering the varieties of constrain limits and aerodynamics deviation, an improved SQP algorithm is used for on-board trajectory planning. Finally, numerical simulation results show that on-board trajectory planning problems with multiple constrain limits and uncertain aerodynamic coefficient can be solved by SQP effectively.
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多级火箭助推器弹道的机载快速规划方法
提出了一种基于序列二次规划(SQP)的多级火箭助推段机载快速规划制导方法。首先,基于多级火箭模型,采用粒子群优化算法,通过飞行轨迹优化获得初始弹道;其次,考虑约束极限和空气动力学偏差的变化,采用改进的SQP算法进行机载轨迹规划;最后,数值仿真结果表明,该方法可以有效地解决具有多约束极限和不确定气动系数的机载轨迹规划问题。
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