中文

Journal of Applied Sciences >

2013 , Vol. 31 >Issue 4: 434 - 440

DOI: https://doi.org/10.3969/j.issn.0255-8297.2013.04.015

Control and System

Rapid Optimization of Penetration Trajectory for Hypersonic Reentry Vehicle

Expand
  • Department of Control Engineeringm, Naval Aeronautical and Astronautical University,
    Yantai 264001, Shandong Province, China

Received date: 2011-10-19

  Revised date: 2012-04-16

  Online published: 2012-04-16

Fold

Abstract

For penetration trajectory optimization of reentry vehicle with constraints of waypoints and no-fly zones, a multi-phase optimization strategy based on adaptive hp pseudospectral method is proposed. The trajectory optimization model considering waypoints, no-fly zones, heating rate, g-load and dynamic pressure
is given. The associated optimization is converted into a nonlinear programming problem by using the Radau pseudospectral method. The concept of linkage nodes is introduced to deal with constraints of waypoints and no-fly zones. Combined with adaptive distribution of nodes, the above idea is implemented with general pseudospectral optimization software. Simulation results show that the proposed method can capture any discontinuities and smoothness in states and control variables as well as the boundary of no-fly zones, and adapt to solve the optimization problem of penetration trajectory with waypoints and no-fly zones.

Key words： penetration trajectory; adaptive hp pseudospectral; general pseudospectral optimization; hypersonic reentry vehicle

Cite this article

WANG Li-ying, ZHANG You-an, ZHAO Guo-rong, HUANG Jie . Rapid Optimization of Penetration Trajectory for Hypersonic Reentry Vehicle[J]. Journal of Applied Sciences, 2013 , 31(4) : 434 -440 . DOI: 10.3969/j.issn.0255-8297.2013.04.015

References

[1] 李瑜，杨志红，崔乃刚. 洲际助推-滑翔导弹全程突防

弹道优化 [J]. 固体火箭技术，2010, 33(2): 125-130.

LI Yu, YANG Zhihong, CUI Naigang. Optimization of overall penetration trajectory for intercontinental boost-glide missile [J]. Journal of Solid Rocket Technology, 2010, 33(2): 125-130. (in Chinese)

[2] 陈小庆，侯中喜，刘建霞. 高超声速滑翔式飞行器再入 轨迹多目标多约束优化 [J]. 国防科技大学学报，2009, 31(6): 76-83.

CHEN Xiaoqing, HOU Zhongxi, LIU Jianxia. Multi-objective optimization of reentry trajectory for hypersonic glide vehicle with multi-constraints [J]. Journal of national university of defense technology, 2009, 31(6): 76-83. (in Chinese)

[3] TIMOTHY R J. Common aero vehicle autonomous

reentry trajectory optimization satisfying waypoint and no-fly zone constraints [D]. The Faculty Graduate School of Engineering and Management Air Force Institute of Technology, 2007.

[4] WILLIAM J K. Optimal reentry trajectory terminal state

due to variations waypoint locations[D]. Department of Aeronautics and Astronautics Graduate School. 2008.

[5] RAO A V, BENSON D, HUNTINGTON G T, et al(补齐作者). Algorithm 902: GPOPS, a MATLAB software for solving multiple-phase optimal control problems using gauss pseudospectral methods [J]. ACM Transactions on Mathematical Software, 2010, 37(2): 22-39.

[6] 杨希祥，张为华. 基于Gauss伪谱法的固体运载火箭上升段轨迹快速优化研究 [J]. 宇航学报，2011, 32(1): 15-21.

YANG Xixiang, ZHANG Weihua. Rapid optimization of

ascent trajectory for solid launch vehicles based on gauss

pseudospectral method [J]. Journal of Astronautics, 2011,

32(1):15-21. (in Chinese)

[7] GUAN Chengqi, CHEN Cong. Multiphase path- constrained trajectory optimization for the boost-glide vehicle via the Gauss pseudospectral method [J]. Journal of Astronautics. 2010, 31(11): 2512-2518.

[8] GARG D. Advances in global pseudospectral method for optimal control [D]. America: University of Florida, 2011.

[9] DARBY C L, HAGER W W, ANIL V. R. An hp-adaptive pseudospectral method for solving optimal control problems [J]. Optimal control applications and methods. 2011, 32 (4): 476-502.

[10] ZHANG Kenna, CHEN Wanchun. Reentry vehicle constraints optimization [C]//17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference. California, AIAA, 2011: 11-14.
Options
Outlines

/

〈 〉