Adaptive mesh refinement method for optimal control based on Hermite-Legendre-Gauss-Lobatto direct transcription

被引:3
作者
Lei, Humin [1 ]
Liu, Tao [1 ]
Li, Deng [2 ,3 ]
Ye, Jikun [1 ]
机构
[1] Air Force Engn Univ, Air & Missile Def Coll, Xian 710051, Shaanxi, Peoples R China
[2] Shaanxi Normal Univ, Coll Educ, Xian 710062, Shaanxi, Peoples R China
[3] Nanyang 2 High Sch, Nanyang 473000, Peoples R China
基金
中国国家自然科学基金;
关键词
optimal control; mesh refinement; relative error estimation; merge mesh intervals; mesh iteration; TRAJECTORY OPTIMIZATION; FRAMEWORK;
D O I
10.21595/jve.2017.18146
中图分类号
R318 [生物医学工程];
学科分类号
0831 ;
摘要
Direct transcription has been employed to transcribe the optimal control problem into a nonlinear programming problem. This paper presents a trajectory optimization method based on a combination of the direct transcription and mesh refinement algorithm. Hermite-Simpson method has the advantage of reasonable accuracy with highly sparse Hessian matrix and constraint Jacobians, and the pseudospectral method provides spectral accuracy for optimal control problems. The optimal control problem is discretized at a series of Legendre-Gauss-Lobatto points, then the trajectory states are approximated by using local Hermite interpolating polynomials. Thus, the method produces significantly smaller mesh size with a higher accuracy tolerance solution. The derived relative error estimation is then used to trade the number of mesh polynomials degree within each mesh interval with the number of mesh intervals. As a result, the suggested method can produce more small mesh size, requires less computation solution for the same optimal control problem. The simulation experiment results show that the suggested method has many advantages.
引用
收藏
页码:6036 / 6048
页数:13
相关论文
共 19 条
  • [1] Survey of numerical methods for trajectory optimization
    Betts, JT
    [J]. JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1998, 21 (02) : 193 - 207
  • [2] Boost-skipping trajectory optimization for air-breathing hypersonic missile
    Chai, Dong
    Fang, Yang-Wang
    Wu, You-li
    Xu, Su-hui
    [J]. AEROSPACE SCIENCE AND TECHNOLOGY, 2015, 46 : 506 - 513
  • [3] THE PSEUDOSPECTRAL LEGENDRE METHOD FOR DISCRETIZING OPTIMAL-CONTROL PROBLEMS
    ELNAGAR, G
    KAZEMI, MA
    RAZZAGHI, M
    [J]. IEEE TRANSACTIONS ON AUTOMATIC CONTROL, 1995, 40 (10) : 1793 - 1796
  • [4] Direct trajectory optimization and costate estimation of finite-horizon and infinite-horizon optimal control problems using a Radau pseudospectral method
    Garg, Divya
    Patterson, Michael A.
    Francolin, Camila
    Darby, Christopher L.
    Huntington, Geoffrey T.
    Hager, William W.
    Rao, Anil V.
    [J]. COMPUTATIONAL OPTIMIZATION AND APPLICATIONS, 2011, 49 (02) : 335 - 358
  • [5] Gill P.E., 2015, User's guide for snopt version 7: Software for large-scale nonlinear programming
  • [6] Gonzalez Arribas Daniel, 2015, IFAC - Papers Online, V48, P192, DOI 10.1016/j.ifacol.2015.08.082
  • [7] Direct optimization using collocation based on high-order Gauss-Lobatto quadrature rules
    Herman, AL
    Conway, BA
    [J]. JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1996, 19 (03) : 592 - 599
  • [8] Hu Y. Q., ACTA AUTOMATICA SINC, V39, P1996
  • [9] Huntington G., 2007, P AIAA GUID NAV CONT
  • [10] Huntington G. T., 2007, ADV ANAL GAUSS PSEUD