摘要
讨论了一种基于高阶Gauss-LobatoQuadrature定律的最优控制直接解法,使用这种方法求解了不可变推力和可变推力两种情况下空间变轨的最优化过程,给出算例。
The direct optimization using collocation based on high order Gauss Lobatto Quadrature rules was discussed.It is a high accuracy and small calculation method.Presently,relative low order rules from the Guass Lobatto rules,such as the trapezoid and Simpson method,were used to construct collocation solution schemes.The advantages of high order scheme are more accuracy and less subintervals which make calculation more quickly.Trajectory optimizations were calculated and several key problems were discussed
出处
《推进技术》
EI
CAS
CSCD
北大核心
1998年第4期66-69,共4页
Journal of Propulsion Technology
关键词
轨道转移
转移轨道计算
最优设计
飞行器
弹道
Orbital transfer,Transfer orbit calculation,Optimum design,Numerical calculation