6-DOF mutual synchronization of formation flying spacecraft

被引：34

作者：

Krogstad, Thomas R. ^{[1
]}

Gravdahl, Jan Tommy ^{[1
]}

机构：

[1] Norwegian Univ Sci & Technol, Dept Engn Cybernet, N-7034 Trondheim, Norway

来源：

PROCEEDINGS OF THE 45TH IEEE CONFERENCE ON DECISION AND CONTROL, VOLS 1-14 | 2006年

关键词：

D O I：

10.1109/CDC.2006.376725

中图分类号：

TP [自动化技术、计算机技术];

学科分类号：

0812 ;

摘要：

In this paper we present a 6 degrees of freedom (6-DOF) synchronization scheme for a deep space formation of spacecraft. In the design, which is referred to as a mutual synchronization scheme, feedback interconnections are designed in such a way that the spacecraft track a time varying reference trajectory while at the same time keep a prescribed relative attitude and position. The closed-loop system is proven uniformly locally asymptotically stable, with an area of attraction which covers the complete state-space, except when the spacecraft attains an attitude where the inverse kinematics are undefined. The proof is carried out using Matrosov's Theorem.

引用

页码：5706 / 5711

页数：6

共 25 条

[11]

Khalil HK., 2002, Nonlinear Systems, V3

[12]

KROGSTAD TR, 2005, P 2005 INT ASTR C OC

[13]

LAWTON JRT, 2000, THESIS BRINGHAM YOUN

[14] High precision formation control of mobile robots using virtual structures [J].

Lewis, MA ;

Tan, KH .

AUTONOMOUS ROBOTS, 1997, 4 (04) :387-403

[15]

MALI AD, 2002, IEEE T SYSTEM MAN C, V32

[16]

MATARIC MJ, 1992, 1992 IEEE INTERNATIONAL CONF ON ROBOTICS AND AUTOMATION : PROCEEDINGS, VOLS 1-3, P830, DOI 10.1109/ROBOT.1992.220192

[17]

Matrosov VM, 1962, Journal of Applied Mathematics and Mechanics, V26, P1337, DOI DOI 10.1016/0021-8928(62)90010-2

[18]

MOREIRA A, 2004, P INT GEOSC REM SENS, V2, P1000

[19]

Nijmeijer H., 2003, SYNCHRONIZATION MECH

[20]

*OHB SYST AG, SAR LUP INN PROGR SA

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