Dual-Quaternion-Based Spacecraft Autonomous Rendezvous and Docking Under Six-Degree-of-Freedom Motion Constraints

This paper addresses the integrated attitude and position control problem for the final phase proximity operations of spacecraft autonomous rendezvous and docking, in which important motion constra...

[1]  Qinglei Hu,et al.  6 DOF synchronized control for spacecraft formation flying with input constraint and parameter uncertainties. , 2011, ISA transactions.

[2]  Shenmin Song,et al.  Safe Guidance for Autonomous Rendezvous and Docking with a Non-Cooperative Target , 2010 .

[3]  Fredrik Nilsson,et al.  PRISMA : an in-orbit test bed for guidance, navigation, and control experiments , 2009 .

[4]  Haiyan Hu,et al.  Output consensus and collision avoidance of a team of flexible spacecraft for on-orbit autonomous assembly , 2016 .

[5]  Panagiotis Tsiotras,et al.  Peer-to-Peer Refueling for Circular Satellite Constellations , 2005 .

[6]  Eric Rogers,et al.  Explicit Model Predictive Control Approach for Low-Thrust Spacecraft Proximity Operations , 2014 .

[7]  I. Garcia,et al.  Trajectory optimization for satellite reconfiguration maneuvers with position and attitude constraints , 2005, Proceedings of the 2005, American Control Conference, 2005..

[8]  Ping Lu,et al.  Solving Nonconvex Optimal Control Problems by Convex Optimization , 2014 .

[9]  Le-ping Yang,et al.  Nonlinear 6-DOF control of spacecraft docking with inter-satellite electromagnetic force , 2012 .

[10]  Gary Slater,et al.  Collision Avoidance for Satellites in Formation Flight , 2004 .

[11]  Ping Lu,et al.  Autonomous Trajectory Planning for Rendezvous and Proximity Operations by Conic Optimization , 2012 .

[12]  Mehran Mesbahi,et al.  Dual Quaternion based Spacecraft Rendezvous with Rotational and Translational Field of View Constraints , 2014 .

[13]  N. K. Philip,et al.  Relative position and attitude estimation and control schemes for the final phase of an autonomous docking mission of spacecraft , 2003 .

[14]  LIANG SUN,et al.  6-DOF integrated adaptive backstepping control for spacecraft proximity operations , 2015, IEEE Transactions on Aerospace and Electronic Systems.

[15]  Clifford,et al.  Preliminary Sketch of Biquaternions , 1871 .

[16]  Youmin Zhang,et al.  Tracking control of spacecraft formation flying with collision avoidance , 2015 .

[17]  Panagiotis Tsiotras,et al.  Pose tracking without linearand angular-velocity feedback using dual quaternions , 2016, IEEE Transactions on Aerospace and Electronic Systems.

[18]  Maruthi R. Akella,et al.  Precision Attitude Stabilization: Incorporating Rise and Fall Times in Gas-Based Thrusters , 2011 .

[19]  Ming Liu,et al.  Finite-Time Control for Spacecraft Formation with Dual-Number-Based Description , 2012 .

[20]  E. Study.  Von den Bewegungen und Umlegungen , 1891 .

[21]  Guangfu Ma,et al.  Dual-Quaternion-Based Fault-Tolerant Control for Spacecraft Tracking With Finite-Time Convergence , 2017, IEEE Transactions on Control Systems Technology.

[22]  Kamesh Subbarao,et al.  Adaptive Output Feedback Control for Spacecraft Rendezvous and Docking Under Measurement Uncertainty , 2006 .

[23]  Panagiotis Tsiotras,et al.  Adaptive Position and Attitude Tracking Controller for Satellite Proximity Operations using Dual Quaternions , 2015 .

[24]  Qinglei Hu,et al.  Dual-quaternion based fault-tolerant control for spacecraft formation flying with finite-time convergence. , 2016, ISA transactions.

[25]  Toru Kasai,et al.  Result of Autonomous Rendezvous Docking Experiment of Engineering Test Satellite-VII , 2001 .

[26]  Daniel E. Koditschek,et al.  Exact robot navigation using artificial potential functions , 1992, IEEE Trans. Robotics Autom..

[27]  Mehran Mesbahi,et al.  Constrained Autonomous Precision Landing via Dual Quaternions and Model Predictive Control , 2017 .

[28]  Huijun Gao,et al.  Guaranteed Cost Output Tracking Control for Autonomous Homing Phase of Spacecraft Rendezvous , 2011 .

[29]  George Vukovich,et al.  Dual-quaternion-based adaptive motion tracking of spacecraft with reduced control effort , 2016 .

[30]  Xianghua Wang,et al.  Fault-Tolerant Attitude Control for Rigid Spacecraft Without Angular Velocity Measurements , 2019, IEEE Transactions on Cybernetics.

[31]  Jonathan P. How,et al.  Safe Trajectories for Autonomous Rendezvous of Spacecraft , 2006 .

[32]  John L. Crassidis,et al.  Attitude estimation for large field-of-view sensors , 2006 .