Time-fuel optimal pulse traversal method for relative orbit spacecraft

Relative orbit transfer and on-orbit target observation are important contents of spacecraft on-orbit service, and it is also required to conform the optimal control performance index. In this paper, a time-fuel optimal pulse traversal method is proposed. It divides the space around the target spacecraft into several spatial grids and the spacecraft traverses the subdivision grids under pulse control. The orbit optimal control and on-orbit observation tasks realize. Finally, the simulation is simulated and the performance indexes of different traversal order are compared.

[1]  A novel algorithm for optimal design of impulsive orbit transfer using multi-phase Gauss pseudospectral method , 2010, 2010 3rd International Symposium on Systems and Control in Aeronautics and Astronautics.

[2]  Jianjun Luo,et al.  Observation trajectory design and control of on-orbit inspection satellite , 2005, International Conference on Space Information Technology.

[3]  Richard Epenoy,et al.  Fuel Optimization for Continuous-Thrust Orbital Rendezvous with Collision Avoidance Constraint , 2011 .

[4]  J. Ross,et al.  Configurable spacecraft control architectures for on-orbit servicing and upgrading of long life orbital platforms , 2004, 2004 IEEE Aerospace Conference Proceedings (IEEE Cat. No.04TH8720).

[5]  Yanchao Sun,et al.  Distributed finite-time configuration containment control for satellite formation , 2017 .

[6]  Cao Xibin,et al.  On-Orbit-Servicing Spacecraft Flyaround Orbit Design and LQR Keep Control in Eccentric Orbits , 2007, 2007 2nd IEEE Conference on Industrial Electronics and Applications.

[7]  A. Ichikawa,et al.  Optimal Impulsive Relative Orbit Transfer Along a Circular Orbit , 2008 .

[8]  Anil V. Rao,et al.  Minimum-Fuel Low-Earth Orbit Aeroassisted Orbital Transfer of Small Spacecraft , 2011 .

[9]  Anil V. Rao,et al.  Minimum-Time Trajectory Optimization of Multiple Revolution Low-Thrust Earth-Orbit Transfers , 2015 .

[10]  Feng Wang,et al.  Attitude tracking control of on-orbit-servicing spacecraft based on eigenaxis maneuver , 2008, 2008 2nd International Symposium on Systems and Control in Aerospace and Astronautics.

[11]  Chuanjiang Li,et al.  On Spacecraft Relative Orbital Motion Based on Main-Flying Direction Method , 2014, ICIC.

[12]  D. Gu,et al.  Optimal orbit transfer of spacecraft under constant thrust , 2016, 2016 Chinese Control and Decision Conference (CCDC).