Dynamics and control during slewing maneuvers-Reference-Cited by-同舟云学术

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Dynamics and control during slewing maneuvers

Published:1989-02 Issue:2 Volume:19 Page:125-143
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Mah H.W.,Modi V.J.,Morita Y.,Yokota H.

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference3 articles.

1. On the dynamics of spacecraft with a slewing appendage;Mah,1986

2. Dynamics of a flexible orbiting platform with MRMS;Morita,1987

3. A mathematical problem and a Spacecraft Control Laboratory Experiment (SCOLE) used to evaluate control laws for flexible spacecraft;Taylor;NASA/IEEE Design Challenge,1984

Cited by 12 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. A stability analysis of a mobile base robot with an energy function;International Journal of Machine Tools and Manufacture;1997-02

2. A composite control scheme for joint tracking and active vibration suppression of mobile flexible manipulator systems;Acta Astronautica;1995-09

3. Non-linear decoupling control of a flexible space platform;Acta Astronautica;1995-01

4. Analytical solution of attitude motion for spacecraft with a slewing appendage;Nonlinear Dynamics;1994-09

5. Nonlinear control of flexible, articulated spacecraft - Application to Space Station/Mobile Manipulator;Journal of Guidance, Control, and Dynamics;1994-01

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