No AccessTriangle Formation Design in Eccentric Orbits Using Pseudospectral Optimal ControlQi Gong, Isaac Ross and Terry AlfriendQi GongUniversity of Texas at San AntonioSearch for more papers by this author, Isaac RossNaval Postgraduate SchoolSearch for more papers by this author and Terry AlfriendTexas A&M UniversitySearch for more papers by this authorSession: ASC-30: Formation FlyingPublished Online:15 Jun 2012https://doi.org/10.2514/6.2008-7360SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookXLinked InRedditEmail About Previous chapter Next chapter FiguresReferencesRelatedDetailsSee PDF for referencesCited byAdaptive dynamic event-triggered deployment control for space triangle tethered formation system with external disturbance1 Nov 2022 | Acta Astronautica, Vol. 200Improved Adaptive Sliding Mode Control for Rigid Spacecraft Attitude Tracking1 Jul 2014 | Journal of Aerospace Engineering, Vol. 27, No. 4Modified Mixed Integer Linear Program for Airport Departure SchedulingSu W. Bae, Jong Park and John-Paul Clarke15 August 2013Trajectory Optimization for Guided Store SeparationRyan Carter and Rick Lind6 September 2012Optimal Control of Relative Motion in Arbitrary Fields: Application at Deimos16 March 2014 | The Journal of the Astronautical Sciences, Vol. 59, No. 1-2 What's Popular AIAA/AAS Astrodynamics Specialist Conference and Exhibit 18 August 2008 - 21 August 2008Honolulu, Hawaiihttps://doi.org/10.2514/6.2008-7360 Crossmark TopicsAerospace SciencesAstrodynamicsAstronauticsComputational Fluid DynamicsFluid DynamicsNumerical AnalysisNumerical InterpolationOrbital ManeuversOrbital PropertyPseudospectral MethodsSpace OrbitStructural Design and DevelopmentStructural Kinematics and DynamicsStructures, Design and Test KeywordsEccentric OrbitPseudospectral Optimal ControlNonlinear DynamicsDistributed Space SystemsLegendre Pseudospectral MethodPropellantSatellite FormationElliptical OrbitSpacecraft FormationGaussian QuadratureDigital Topics Astrodynamics