Fuel-Optimal Spacecraft Rendezvous with Hybrid On-Off Continuous and Impulsive Thrust
Author:
Affiliation:
1. University of Rome “La Sapienza”, 00161 Rome, Italy
2. U.S. Naval Postgraduate School, Monterey, California 93943
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/10.2514/1.27716
Reference14 articles.
1. Fuel-optimal maneuvers of a spacecraft relative to a point in circular orbit
2. Fuel-optimal rendezvous for linearized equations of motion
3. Optimal power-limited rendezvous with upper and lower bounds on thrust
4. Optimal Bounded Low-Thrust Rendezvous with Fixed Terminal-Approach Direction
5. Optimal Relocation of Satellites Flying in Near-Circular-Orbit Formations
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