Nonlinear optimal attitude control of spacecraft using novel state-dependent coefficient parameterizations
Junyu Yao, Qinglei Hu, Jianying Zheng
Topics & Concepts
QuaternionPointwiseControl theory (sociology)Nonlinear systemRiccati equationComputer scienceScalar (mathematics)SpacecraftAttitude controlNoveltyControl (management)MathematicsMathematical optimizationControl engineeringEngineeringAerospace engineeringArtificial intelligenceMathematical analysisPhysicsPhilosophyGeometryDifferential equationTheologyQuantum mechanicsAdaptive Control of Nonlinear SystemsSpacecraft Dynamics and ControlDynamics and Control of Mechanical Systems