Successive Convexification for Satellite Swarms Trajectory Planning and Collision Avoidance
Author:
Affiliation:
1. Shandong Institute of Space Electronic Technology,Yantai,P.R. China,264000
2. Harbin Institute of Technology,Research Center of Satellite Technology,Harbin,P.R. China,150001
3. China Academy of Launch Vehicle Technology,Beijing,P.R. China,100076
Funder
National Natural Science Foundation of China
National Key R&D Program of China
China Postdoctoral Science Foundation
Publisher
IEEE
Link
http://xplorestaging.ieee.org/ielx7/10239690/10239711/10240351.pdf?arnumber=10240351
Reference19 articles.
1. Enhanced Successive Convexification Based on Error-Feedback Index and Line Search Filter
2. Convex Optimization
3. Successive Convexification for Ascent Trajectory Replanning of a Multi-stage Launch Vehicle Experiencing Non-fatal Dynamic Faults
4. Fuel-Optimal Low-Thrust Trajectory Optimization Using Indirect Method and Successive Convex Programming
5. Spacecraft Trajectory Planning with Avoidance Constraints Using Mixed-Integer Linear Programming
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