摘要
研究了导弹在末制导阶段满足多约束条件下的轨迹优化问题。针对传统方法在处理复杂的非线性运动学、动力学约束上存在的困难,提出了一种基于Radau伪谱方法(RPM)的求解策略。首先,给出了考虑导弹速度和空气密度变化、终端和过程约束条件以及2种不同的性能指标函数的最优轨迹优化问题;其次,利用RPM将轨迹优化问题转化为非线性规划问题,采用序列二次规划算法求得最优解;最后,分2种初始条件对最大落角和最大终端速度的轨迹优化问题进行了仿真验证,结果表明:本文方法能够在较短的时间内生成一条满足多种约束要求的高精度的最优轨迹。
Trajectory optimization problem of missile which satisfies multi-constraints in the terminal phase was studied in this paper. In order to deal with the difficulties of traditional method in processing complicated nonlinear kinematic and dynamic constraints, a strategy which based on Radau pseudospectral method（RPM）was proposed. Firstly, trajectory optimization problem was given which took into consideration missile velocity and air density changing, terminal and process constraints and two different performance indexes. Secondly, trajectory optimization problem was transformed into a nonlinear programming problem using RPM, which could be solved using a sequential quadratic programming algorithm. Finally, numerical validation for maximum terminal impact angle and maximum terminal velocity of trajectory optimization problem in two difference initial conditions were used to demonstrate effectiveness of the proposed algorithm. The results showed that the optimal trajectory which satisfied mult-constraints conditions could be obtained with short time and good precision in this paper.
出处
《海军航空工程学院学报》
2015年第4期315-320,共6页
Journal of Naval Aeronautical and Astronautical University
基金
国家自然科学基金资助项目(61273058)
关键词
Radau伪谱方法
多约束条件
最优控制
轨迹优化
末制导
Radau pseudospectral method
multi-constraints condition
optimal control
trajectory optimization
terminal guidance
