Volume 40 Issue 4
Jul.  2020
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SUN Zhiyuan, LIU Zhiyong, ZHANG Peng. Mars Entry Trajectory Quick Optimization Method for Lifting Vehicle Based on Adaptive GPM[J]. Journal of Space Science, 2020, 40(4): 547-553. doi: 10.11728/cjss2020.04.547
Citation: SUN Zhiyuan, LIU Zhiyong, ZHANG Peng. Mars Entry Trajectory Quick Optimization Method for Lifting Vehicle Based on Adaptive GPM[J]. Journal of Space Science, 2020, 40(4): 547-553. doi: 10.11728/cjss2020.04.547

Mars Entry Trajectory Quick Optimization Method for Lifting Vehicle Based on Adaptive GPM

doi: 10.11728/cjss2020.04.547
  • Received Date: 2019-04-26
  • Rev Recd Date: 2019-12-06
  • Publish Date: 2020-07-15
  • A new method is given based on adaptive Gauss pseudospectral method for quick trajectory optimization problem of Mars entry. This method converts the trajectory optimization problem to a non-linear programming problem, taking into account for the dynamic constrains, the boundary constrains, the path constrains and the control constrains during the Mars entry of the lifting vehicle. And then, sequential quadratic programming is adapted to solve the non-linear programming problem, and the optimal fuel-consuming trajectory is obtained. In combination with the adaptive Gauss pseudospectral method and sequential quadratic programming in Matlab software, the numerical results of the optimal trajectory with 267 collocations could be obtained in 800s with an approximation accuracy of 10-6. The numerical results are smooth and meet all constrains during the Mars entry process, which suggests that the method introduced in this paper is available and of great practical application.

     

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  • [1]
    JARRET M L, JOHN R O, ROBERT D B. Daedalon:A Revolutionary Morphing Spacecraft Design for Planetary Exploration[C]//1st Space Exploration Conference:Continuing the Voyage of Discovery. Orlando:AIAA, 2005
    [2]
    YONG Enmi, CHEN Lei, TANG Guojin. A survey of numerical methods for trajectory optimization of spacecraft[J]. J. Astronaut., 2008, 29(2):397-406
    [3]
    CHEN Cong, GUAN Chengqi, SHI Hongliang. Survey of numerical methods for direct aircraft trajectory optimization[J]. Control Tech. Tactical Missile, 2009, 31(2):33-40
    [4]
    BENSON D A, HUNTINGTOM G T. Direct trajectory optimization and costate estimation via an orthogonal collocation method[J]. J. Guid. Control Dynam., 2006, 29(6):1435-1440
    [5]
    YANG Xixiang, ZHANG Weihua. Rapid optimization of ascent trajectory for solid launch vehicles based on Gauss pseudospectral method[J]. J. Astronaut., 2011, 32(1):15-21
    [6]
    ZHOU Wenya, YANG Di, LI Shunli. Using Gauss pseudospectral method to solve optimal reentry trajectory for lifting vehicle[J]. J. Nanjing Univ. Sci. Tech.:Natl. Sci., 2010, 34(1):85-90
    [7]
    PENG Qibo, LI Haiyang, SHEN Hongxin. Rapid lunar exact-landing trajectory optimization via gauss pseudospectral method[J]. J. Astronaut., 2010, 31(4):1012-1016
    [8]
    HUNTINGTON G T. Optimal reconfiguration of spacecraft formations using a Gauss pseudospectral method[J]. J. Guid. Control Dynam., 2008, 31(3):689-698
    [9]
    DARBY C L, HAGER W W, RAO A V. An hp-adaptive pseudospectral method for solving optimal control problems[J]. Optim. Control Appl. Methods, 2011, 32(4):476-502
    [10]
    VINH N X. Optimal Trajectories in Atmospheric Flight[M]. New York:Elsevier Scientific Publishing Co., 1981
    [11]
    ZENG Xiangxin, CUI Naigang, GUO Jifeng. Path planning of space robot based on hp-adaptive pseudospectral method[J]. Robot, 2018, 40(3):342-385
    [12]
    LIU Ruifan, YU Yunfeng, YAN Binbin. Ascent phase trajectory optimization for hypersonic vehicle based on hp-adaptive pseudospectral method[J]. J. Northwestern Polytech. Univ., 2016, 10(5):790-797
    [13]
    BENITO M J. Advances in Spacecraft Atmospheric Entry Guidance[D]. California:University of California, 2010
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