No AccessSpacecraft large angle rotational maneuvers with optimal momentum transferS. VADALI and J. JUNKINSS. VADALIVirginia Polytechnic Institute and State University, Blacksburg, VASearch for more papers by this author and J. JUNKINSVirginia Polytechnic Institute and State University, Blacksburg, VASearch for more papers by this authorPublished Online:17 Aug 2012https://doi.org/10.2514/6.1982-1469SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About Previous chapter Next chapter FiguresReferencesRelatedDetailsSee PDF for referencesCited byOptimal Configuration of Four Reaction Wheels in Momentum Management Performance and Reliability Point of View1 March 2023 | Iranian Journal of Science and Technology, Transactions of Mechanical Engineering, Vol. 47, No. 4Closed-form solution of attitude command generation for spin-to-spin maneuverAdvances in Space Research, Vol. 71, No. 1Inverse dynamics particle swarm optimization applied to constrained minimum-time maneuvers using reaction wheelsAerospace Science and Technology, Vol. 75Nonlinear momentum transfer control of a gyrostat with a discrete damper using neural networksActa Astronautica, Vol. 62, No. 6-7Nonlinear Momentum Transfer Control of a Gyrostat with a Discrete Damper by Using Neural NetworksNonlinear Momentum Transfer Control by Using Neural NetworksHyunjae Lee, Hyochoong Bang, Min-Jea Tahk and Kun Tae Kim22 June 2012Nonlinear Momentum Transfer Control of Spacecraft by Feedback Linearization Hyochoong Bang , Hyun-Sam Myung and Min-Jea Tahk 23 May 2012 | Journal of Spacecraft and Rockets, Vol. 39, No. 6Nonlinear Momentum Transfer Control of Spacecraft by Feedback LinearizationHyochoong Bang, Hyun-Sam Myung and Min-Jea Tahk25 June 2012Exact feedback linearization and control of space station using CMGIEEE Transactions on Automatic Control, Vol. 38, No. 1Nonlinear adaptive attitude control of satellite using gyrotorquersVariable-structure control of spacecraft attitude maneuvers Thomas A. W. Dwyer III and Hebertt Sira-Ramirez 23 May 2012 | Journal of Guidance, Control, and Dynamics, Vol. 11, No. 3Minimum time slewing of the SIRTF spacecraftN. RAJAN17 August 2012Exact nonlinear control of spacecraft slewing maneuvers with internal momentum transfer Thomas A.W. Dwyer III 23 May 2012 | Journal of Guidance, Control, and Dynamics, Vol. 9, No. 2Optimal Maneuvers of Rigid SpacecraftExact nonlinear control of spacecraft slewing maneuvers with internal momentum transferT. DWYER, III17 August 2012The optimal control of flexible systems using a convolution integral description of motionAlgebraic computations for design of nonlinear control systemsDesign of nonlinear control systems using CONDENS What's Popular Astrodynamics Conference 09 August 1982 - 11 August 1982San Diego,CA,U.S.A.https://doi.org/10.2514/6.1982-1469 Crossmark TopicsBoundary Element MethodComputational Fluid DynamicsFluid DynamicsNumerical AnalysisRunge-Kutta MethodsSpace Systems and VehiclesSpacecrafts KeywordsSpacecraftsNewton Raphson MethodAstrodynamicsBoundary Value ProblemsRunge Kutta MethodsReaction WheelsPDF Topics Astrodynamics