Particle Swarm Optimization for Time-Optimal Spacecraft Reorientation with Keep-Out Cones-Reference-Cited by-同舟云学术

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Particle Swarm Optimization for Time-Optimal Spacecraft Reorientation with Keep-Out Cones

Published:2016-02 Issue:2 Volume:39 Page:312-325
ISSN:0731-5090
Container-title:Journal of Guidance, Control, and Dynamics
language:en
Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Spiller Dario¹,Ansalone Luigi²,Curti Fabio³

Affiliation:

1. University of Rome “La Sapienza”, 00184 Rome, Italy

2. Technology Division, Agenzia Spaziale Italiana, 00133 Rome, Italy

3. School of Aerospace Engineering, Laboratory of Automation, Robotics and Control for Aerospace, University of Rome “La Sapienza”, 00138 Rome, Italy

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/10.2514/1.G001228

Reference43 articles.

1. Time-optimal three-axis reorientation of a rigid spacecraft

2. Numerical approach for solving rigid spacecraft minimum time attitude maneuvers

3. Survey of time-optimal attitude maneuvers

4. Quasi-closed-form solution to the time-optimal rigid spacecraft reorientation problem

5. Time-Optimal Control of Axisymmetric Rigid Spacecraft Using Two Controls

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