Title :
Attitude consensus using quaternion-based controller composing augmented dynamic
Author :
Septanto, Harry ; Bambang, Riyanto T. ; Syaichu-Rohman, Arief ; Poetro, Ridanto Eko
Author_Institution :
Sch. of Electr. Eng. & Inf., Inst. Teknol. Bandung, Bandung, Indonesia
Abstract :
Nonlinearity of dynamics and kinematics, difficulty in stability guarantee and unwinding phenomenon problem make quaternion-based attitude control system design is a non trivial problem. The non triviality is increase in the design of attitude consensus of rigid bodies in a group. This paper provides a distributed controller that depends on information-state for attitude consensus among a group of rigid bodies. The controller is developed based on continuous quaternion-based attitude controller composing augmented dynamic. The designed attitude consensus has global motion to rest and rest to rest maneuver properties. Simulation run verifies that unwinding phenomenon can be avoided.
Keywords :
attitude control; control nonlinearities; distributed control; mechanical stability; space vehicles; vehicle dynamics; attitude consensus design; augmented dynamic composition; continuous quaternion-based attitude controller; distributed controller; dynamics nonlinearity; global motion-to-rest maneuver property; information-state; kinematics nonlinearity; nontrivial problem; quaternion-based attitude control system design; rest-to-rest maneuver property; single spacecraft control design; stability guarantee; unwinding phenomenon problem; Aerodynamics; Attitude control; Kinematics; Quaternions; Space vehicles; Topology; Attitude consensus; augmented dynamic; motion to rest and rest to rest maneuvers; quaternion; unwinding phenomenon;
Conference_Titel :
System Engineering and Technology (ICSET), 2014 IEEE 4th International Conference on
Print_ISBN :
978-1-4799-7188-6
DOI :
10.1109/ICSEngT.2014.7111794