Receding horizon guidance and control using sequential convex programming for spacecraft 6-DOF close proximity

Author:

Zhou Ding,Zhang Yanquan,Li Shunli

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference45 articles.

1. Relative motion coupled control for formation flying spacecraft via convex optimization;Wu;Aerosp. Sci. Technol.,2010

2. Spacecraft Formation Flying: Dynamics, Control and Navigation;Alfriend,2008

3. Spiral coning manoeuvre for in-orbit low thrust characterisation in cubesats;Macario-Rojas;Aerosp. Sci. Technol.,2017

4. Trajectory planning for cubesat short-time-scale proximity operations;Kobilarov;J. Guid. Control Dyn.,2014

5. Tube-based robust model predictive control for spacecraft proximity operations in the presence of persistent disturbance;Mammarella;Aerosp. Sci. Technol.,2018

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