Optimal control of orbit transfer of space probe with finite thrust

Xingsuo He; Ping Wang; Jianping Yuan; Shengyong Lin

Optimal control of orbit transfer of space probe with finite thrust

Xingsuo He
, Ping Wang
, Jianping Yuan
, Shengyong Lin

School of Astronautics

Northwestern Polytechnical University Xian

Research output: Contribution to conference › Paper › peer-review

Abstract

The minimum-fuel orbit transfer with finite thrust is studied here. The optimization of the dynamic equations including the control parameters shows that the optimal values are constants. The initial true anomaly f₀, yaw angle ψ and the dive angle φ are selected as the start values of the iteration method. And the constraint conditions in the Two-point Boundary Value Problems are presented. Finally, two numerical examples of optimal orbit transfer are calculated and discussed. The results showing the optimal method in the paper is feasible.

Original language	English
Pages	1017-1022
Number of pages	6
State	Published - 2005
Event	International Astronautical Federation - 56th International Astronautical Congress 2005 - Fukuoka, Japan Duration: 17 Oct 2005 → 21 Oct 2005

Conference

Conference	International Astronautical Federation - 56th International Astronautical Congress 2005
Country/Territory	Japan
City	Fukuoka
Period	17/10/05 → 21/10/05

Keywords

Finite thrust
Optimal control
Orbit transfer

Cite this

@conference{b10be5ac849c4f07ac42a78ba7736b71,

title = "Optimal control of orbit transfer of space probe with finite thrust",

abstract = "The minimum-fuel orbit transfer with finite thrust is studied here. The optimization of the dynamic equations including the control parameters shows that the optimal values are constants. The initial true anomaly f0, yaw angle ψ and the dive angle φ are selected as the start values of the iteration method. And the constraint conditions in the Two-point Boundary Value Problems are presented. Finally, two numerical examples of optimal orbit transfer are calculated and discussed. The results showing the optimal method in the paper is feasible.",

keywords = "Finite thrust, Optimal control, Orbit transfer",

author = "Xingsuo He and Ping Wang and Jianping Yuan and Shengyong Lin",

year = "2005",

language = "英语",

pages = "1017--1022",

note = "International Astronautical Federation - 56th International Astronautical Congress 2005 ; Conference date: 17-10-2005 Through 21-10-2005",

}

TY - CONF

T1 - Optimal control of orbit transfer of space probe with finite thrust

AU - He, Xingsuo

AU - Wang, Ping

AU - Yuan, Jianping

AU - Lin, Shengyong

PY - 2005

Y1 - 2005

N2 - The minimum-fuel orbit transfer with finite thrust is studied here. The optimization of the dynamic equations including the control parameters shows that the optimal values are constants. The initial true anomaly f0, yaw angle ψ and the dive angle φ are selected as the start values of the iteration method. And the constraint conditions in the Two-point Boundary Value Problems are presented. Finally, two numerical examples of optimal orbit transfer are calculated and discussed. The results showing the optimal method in the paper is feasible.

AB - The minimum-fuel orbit transfer with finite thrust is studied here. The optimization of the dynamic equations including the control parameters shows that the optimal values are constants. The initial true anomaly f0, yaw angle ψ and the dive angle φ are selected as the start values of the iteration method. And the constraint conditions in the Two-point Boundary Value Problems are presented. Finally, two numerical examples of optimal orbit transfer are calculated and discussed. The results showing the optimal method in the paper is feasible.

KW - Finite thrust

KW - Optimal control

KW - Orbit transfer

UR - https://www.scopus.com/pages/publications/34250805882

M3 - 论文

AN - SCOPUS:34250805882

SP - 1017

EP - 1022

T2 - International Astronautical Federation - 56th International Astronautical Congress 2005

Y2 - 17 October 2005 through 21 October 2005

ER -

Optimal control of orbit transfer of space probe with finite thrust

Abstract

Conference

Keywords

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