A quasi-linear local variational iteration method for orbit transfer problems

被引:4
作者
Feng, Haoyang [1 ,2 ]
Yue, Xiaokui [1 ,2 ]
Wang, Xuechuan [1 ,2 ]
机构
[1] Northwestern Polytech Univ, Sch Astronaut, 127 West Youyi Rd, Xian 710072, Peoples R China
[2] Northwestern Polytech Univ, Natl Key Lab Aerosp Flight Dynam, 127 West Youyi Rd, Xian 710072, Peoples R China
基金
中国国家自然科学基金;
关键词
Quasi-linearization; Local variational iteration method; Perturbed Lambert's problem; Two-point boundary value problem; Shooting method; PICARD ITERATION; SHOOTING METHOD; BOUNDARY;
D O I
10.1016/j.ast.2021.107222
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
A novel Quasi-linear Local Variational Iteration Method (QLVIM) for solving two-point boundary value problems (TPBVPs) of strongly nonlinear systems is proposed. With quasi-linearization technique, the multidimensional nonlinear TPBVP is transformed into a series of iterative linear TPBVPs, and then into initial value problems (IVPs) which appear in pairs. Then these IVPs are solved by Local Variational Iteration Method (LVIM). Combining the rapid convergence of quasi-linearization with the high computational efficiency of LVIM, the proposed QLVIM can solve various orbit transfer problems in aerospace engineering efficiently and accurately. The high-performance of this method is verified in solving perturbed Lambert's problems and a circular restricted three-body orbit transfer problem. Comparisons with various methods show that the QLVIM has the advantages of high convergence speed, low computation cost and longer solvable time span. Rather than a refined initial guess of starting velocity, the QLVIM only needs a rough initial guess of the trajectory. The results also prove that the QLVIM is capable of solving long-time-span orbit transfer problem. A theoretical proof of its quadratic convergence is given at last. (c) 2021 Elsevier Masson SAS. All rights reserved.
引用
收藏
页数:16
相关论文
共 37 条
[1]   2-POINT BOUNDARY VALUE PROBLEMS - SHOOTING METHODS - ROBERTS,SM AND SHIPMAN,JS']JS [J].
ANDREW, AL .
TECHNOMETRICS, 1975, 17 (02) :277-278
[2]  
Bai X., 2010, TESIS
[3]  
Battin R.H., 1999, INTRO MATH METHODS A, DOI DOI 10.2514/4.861543
[4]  
Bellman R.E, 1965, QUASILINEARIZATION N, P36
[5]  
ccmc.gsfc.nasa, MSIS E 90 ATMOSPHERE
[6]   Newton-Kantorovich/Pseudospectral Solution to Perturbed Astrodynamic Two-Point Boundary-Value Problems [J].
Chen, Qifeng ;
Zhang, Yuedong ;
Liao, Shouyi ;
Wan, Fanliang .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2013, 36 (02) :485-498
[7]   Reconfiguration control of satellite formation using online quasi-linearization iteration and symplectic discretization [J].
Cheng, Long ;
Wen, Hao ;
Jin, Dongping .
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 107
[8]  
Curtis H., 2020, ORBITAL MECH ENG STU, V4nd, P116
[9]   A time domain collocation method for studying the aeroelasticity of a two dimensional airfoil with a structural nonlinearity [J].
Dai, Honghua ;
Yue, Xiaokui ;
Yuan, Jianping ;
Atluri, Satya N. .
JOURNAL OF COMPUTATIONAL PHYSICS, 2014, 270 :214-237
[10]  
Dong L, 2014, CMES-COMP MODEL ENG, V99, P1