Near-minimum time open-loop slewing of flexible vehicles-Reference-Cited by-同舟云学术

Near-minimum time open-loop slewing of flexible vehicles

Published:1989-01 Issue:1 Volume:12 Page:82-88
ISSN:0731-5090
Container-title:Journal of Guidance, Control, and Dynamics
language:en
Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Thompson R. C.¹,Junkins J. L.¹,Vadali S. R.¹

Affiliation:

1. Texas A&M University, College Station, Texas

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/10.2514/3.20371

Reference10 articles.

1. Design of space structure control systems using on-off thrusters

2. Method of particular solutions for linear, two-point boundary-value problems

3. 4Vadali, S.R. "Solution of the Two-Point Boundary Value Problems of Optimal Spacecraft Rotational Maneuvers,"Ph.D. Dissertation,Virginia Polytechnic Institute and State Univ., Blacksburg, VA, 1982.

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