Continuous Distributed Fixed-Time Attitude Controller Design for Multiple Spacecraft Systems With a Directed Graph
Bing Cui, Lijun Zhang, Yuanqing Xia, Jinhui Zhang
Abstract
This brief addresses the fixed-time leader-following attitude consensus problem for multiple spacecraft systems on a directed graph. A distributed continuous observer is designed to estimate the angular velocity of the leader within a fixed time. Based on the fixed-time observer and adding a power integrator method, a continuous distributed adaptive controller is developed to achieve the consensus tracking control in a fixed time which is regardless of the initial conditions. The proposed continuous fixed-time scheme works well when the systems are subject to model uncertainties and external disturbances. The simulation results show the effectiveness of the proposed control scheme.
Topics & Concepts
Control theory (sociology)Observer (physics)Computer scienceSpacecraftIntegratorGraphFixed wingController (irrigation)ConsensusFixed pointMulti-agent systemControl (management)MathematicsEngineeringBandwidth (computing)Theoretical computer scienceMathematical analysisBiologyAgronomyArtificial intelligenceComputer networkQuantum mechanicsAerospace engineeringPhysicsWingAdaptive Control of Nonlinear SystemsDistributed Control Multi-Agent SystemsMitochondrial Function and Pathology