Inequality constraints in primer-optimal, N-impulse solutions
Author:
Affiliation:
1. NASA Manned Spacecraft Center, Houston, Texas
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.6272
Reference5 articles.
1. Primer vector on fixed-time impulsive trajectories.
2. An efficient method for calculating optimal free-space n-impulse trajectories.
3. A Rapidly Convergent Descent Method for Minimization
4. Impulsive orbit transfer optimization by an accelerated gradient method.
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3. Orbit Transfer Optimization for Asteroid Missions Using Weighted Cost Function;Journal of Guidance, Control, and Dynamics;2015-07
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