Fuel optimal reorientation of axisymmetric spin-stabilized satellites-Reference-Cited by-同舟云学术

Fuel optimal reorientation of axisymmetric spin-stabilized satellites

Published:1993-01 Issue:1 Volume:16 Page:217-219
ISSN:0731-5090
Container-title:Journal of Guidance, Control, and Dynamics
language:en
Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Redmond Jim¹,Silverberg Larry¹

Affiliation:

1. North Carolina State University, Raleigh, North Carolina 27695

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.11449

Reference8 articles.

1. Optimal attitude control of a spinning space-body--A graphical approach

2. Optimal and near-optimal regulation of spacecraft spin axes

3. 4Wingate, R. T. "Fuel-Optimal Reorientation of a Spinning Body," Ph.D. Dissertation, Dept. of Engineering Mechanics,Virginia PolytechnicInst.and State Univ., Blacksburg, VA,July 1970.

4. On the theory of optimum control

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