Constellation Phasing of Spacecraft in Near-Circular, In-Plane Orbits using Low-Thrust Trajectory Optimization
Author:
Affiliation:
1. University of California,Department of Mechanical Engineering,Berkeley
2. University of California,Department of Electrical Engineering & Computer Sciences,Berkeley
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/10155646/10155787/10155863.pdf?arnumber=10155863
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3. Small Satellite Constellation Separation using Linear Programming based Differential Drag Commands
4. Successive convexification: A superlinearly convergent algorithm for non-convex optimal control problems;mao,2019
5. Successive Convexification for Mars 6-DoF Powered Descent Landing Guidance
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