Attitude Consensusability in Multispacecraft Systems Using Magnetic Actuators

The leaderless attitude consensusability of multispacecraft systems by using magnetic actuators is addressed. By proposing a nonlinear consensus protocol for the actuators magnetic dipoles, it is shown that the multispacecraft system is average controllable under the consensus protocol if it is maneuvering at orbits with persistently exciting magnetic fields in the Earth-centered inertial frame. Then, under some conditions, achieving consensus in the multispacecraft system is studied. Simulation results for a team of spacecraft validate the proposed consensus strategy.

[1]  Michael A. Demetriou,et al.  Adaptation of consensus penalty terms for attitude synchronization of spacecraft formation with unknown parameters , 2013, 52nd IEEE Conference on Decision and Control.

[2]  K.Y. Pettersen,et al.  Leader/Follower synchronization of satellite attitude without angular velocity measurements , 2005, Proceedings of the 44th IEEE Conference on Decision and Control.

[3]  Junquan Li,et al.  Decentralized Fault-Tolerant Control for Satellite Attitude Synchronization , 2012, IEEE Transactions on Fuzzy Systems.

[4]  An-Min Zou,et al.  Distributed Attitude Coordination Control for Spacecraft Formation Flying , 2012, IEEE Transactions on Aerospace and Electronic Systems.

[5]  Sanjay P. Bhat,et al.  Controllability of nonlinear time-varying systems: applications to spacecraft attitude control using magnetic actuation , 2005, IEEE Transactions on Automatic Control.

[6]  Wen-Hua Chen,et al.  Variable sampling-time nonlinear model predictive control of satellites using magneto-torquers , 2014 .

[7]  Richard M. Murray,et al.  Consensus problems in networks of agents with switching topology and time-delays , 2004, IEEE Transactions on Automatic Control.

[8]  Yulin Zhang,et al.  Control design and analysis of an inner-formation flying system , 2015, IEEE Transactions on Aerospace and Electronic Systems.

[9]  Itzhak Barkana,et al.  Defending the beauty of the Invariance Principle , 2014, Int. J. Control.

[10]  Peng Shi,et al.  Distributed attitude control for multiple spacecraft with communication delays , 2014, IEEE Transactions on Aerospace and Electronic Systems.

[11]  Andrea Maria Zanchettin,et al.  Robust Magnetic Attitude Control of Satellites , 2013, IEEE/ASME Transactions on Mechatronics.

[12]  Farzaneh Abdollahi,et al.  Pursuit Formation of Double-Integrator Dynamics Using Consensus Control Approach , 2015, IEEE Transactions on Industrial Electronics.

[13]  Alessandro Astolfi,et al.  Spacecraft attitude control using magnetic actuators , 2004, Autom..

[14]  Marco Lovera,et al.  Magnetic satellite detumbling: The b-dot algorithm revisited , 2015, 2015 American Control Conference (ACC).

[15]  A. Astolfi,et al.  Global magnetic attitude control of spacecraft in the presence of gravity gradient , 2003, IEEE Transactions on Aerospace and Electronic Systems.

[16]  Mehran Mesbahi,et al.  Spacecraft synchronization in the presence of attitude constrained zones , 2012, 2012 American Control Conference (ACC).

[17]  Fuchun Sun,et al.  Decentralized adaptive attitude synchronization of spacecraft formation , 2012, Syst. Control. Lett..

[18]  Soon-Jo Chung,et al.  Application of Synchronization to Formation Flying Spacecraft: Lagrangian Approach , 2008, 0803.0170.

[19]  Eric C. Kerrigan,et al.  Suboptimal predictive control for satellite detumbling , 2014 .

[20]  Wei Ren,et al.  Distributed attitude alignment in spacecraft formation flying , 2007 .

[21]  Fabio Celani,et al.  Robust three-axis attitude stabilization for inertial pointing spacecraft using magnetorquers , 2014, 1411.2756.

[22]  Luca Zaccarian,et al.  Reaction Wheels Desaturation Using Magnetorquers and Static Input Allocation , 2015, IEEE Transactions on Control Systems Technology.

[23]  Yaguang Yang Controllability of spacecraft using only magnetic torques , 2016, IEEE Transactions on Aerospace and Electronic Systems.