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
相关论文
共 20 条
[11]  
Betts J.T., Survey of numerical methods for trajectory optimization, Journal of Guidance, Control, and Dynamics, 21, 2, (1998)
[12]  
Acikmese B., Ploen S.R., Convex programming approach to powered descent guidance for mar landing, Journal of Guidance, Control, and Dynamics, 30, 5, (2007)
[13]  
Blackmore L., Acikmese B., Scharf D.P., Minimum-landing-error power-descent guidance for Mars landing using convex optimization, Journal of Guidance, Control, and Dynamics, 33, 4, (2010)
[14]  
Liu X., Shen Z., Lu P., Exact convex relaxation for optimal flight of aerodynamically controlled missiles, IEEE Transaction on Aerospace and Electronic Systems, 52, 4, (2016)
[15]  
Liu X., Shen Z., Lu P., Closed-loop optimization of guidance gain for constrained impact, Journal of Guidance, Control, and Dynamics, 40, 2, (2017)
[16]  
Liu X., Shen Z., Lu P., Entry trajectory optimization by second-order cone programming, Journal of Guidance, Control, and Dynamics, 39, 2, (2016)
[17]  
Szmuk M., Acikmese B., Successive convexification for fuel-optimal powered landing with aerodynamic drag and non-convex constraints, AIAA Guidance, Navigation, and Control Conference, (2016)
[18]  
Mao Y., Szmuk M., Acikmese B., Successive convexification of non-convex optimal control problems and its convergence properties, Conference on Decision and Control , (2016)
[19]  
Szmuk M., Acikmese B., Successive convexification for Mars 6-DOF powered descent landing guidance, AIAA Guidance, Navigation, and Control Conference, (2017)
[20]  
Mao Y., Dueri D., Szmuk M., Acikmese B., Successive convexification of non-convex optimal control problems with state constraints, IFAC Paper OnLine, 50, 1, (2017)