Trajectory optimization for impact angle control based on sequential convex programming

被引:0
作者
Kwon H.-H. [1 ,2 ]
Shin H.-S. [1 ,2 ]
Kim Y.-H. [1 ,2 ]
Lee D.-H. [1 ,2 ]
机构
[1] PGM Lab.
[2] PGM Lab., LIG
关键词
Impact angle control; Second-order cone programming; Sequential convex programming; Trajectory optimization;
D O I
10.5370/KIEE.2019.68.1.159
中图分类号
学科分类号
摘要
- Due to the various engagement situations, it is very difficult to generate the optimal trajectory with several constraints. This paper investigates the sequential convex programming for the impact angle control with the additional constraint of altitude limit. Recently, the SOCP(Second-Order Cone Programming), which is one area of the convex optimization, is widely used to solve variable optimal problems because it is robust to initial values, and resolves problems quickly and reliably. The trajectory optimization problem is reconstructed as convex optimization problem using appropriate linearization and discretization. Finally, simulation results are compared with analytic result and nonlinear optimization result for verification. Copyright © The Korean Institute of Electrical Engineers.
引用
收藏
页码:159 / 166
页数:7
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