No AccessDesign of Launch Vehicle Flight Control Systems Using Ascent Vehicle Stability Analysis ToolJiannwoei Jang, Abran Alaniz, Robert Hall, Nazareth Bedrossian, Charles Hall and Mark JacksonJiannwoei JangDraper LaboratorySearch for more papers by this author, Abran AlanizDraper LaboratorySearch for more papers by this author, Robert HallDraper LaboratorySearch for more papers by this author, Nazareth BedrossianDraper LaboratorySearch for more papers by this author, Charles HallNASA Marshall Space Flight CenterSearch for more papers by this author and Mark JacksonNASA Marshall Space Flight CenterSearch for more papers by this authorPublished Online:14 Jun 2012https://doi.org/10.2514/6.2011-6652SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookXLinked InRedditEmail About Previous chapter Next chapter FiguresReferencesRelatedDetailsSee PDF for referencesCited byADCS Design for a Sounding Rocket with Thrust Vectoring8 July 2023 | Aerotecnica Missili & Spazio, Vol. 102, No. 3Geometrization of Linearization-based Control Laws on the Unit Circle16 Aug 2022A High-Order Load Model and the Control Algorithm for an Aerospace Electro-Hydraulic Actuator7 March 2021 | Actuators, Vol. 10, No. 3Solving of the some special control problems of launch vehicle at the initial flight part using the AKOR method1 Jan 2021LQG Controller for Load Relief Control of a Flexible Launch Vehicle1 Oct 2019Load relief control of launch vehicle using aerodynamic angle estimation23 March 2017 | Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, Vol. 232, No. 8Robust steering control of spacecraft carrier rockets1 Mar 2013 What's Popular AIAA Guidance, Navigation, and Control Conference 08 August 2011 - 11 August 2011Portland, Oregonhttps://doi.org/10.2514/6.2011-6652 Crossmark TopicsAerodynamic PerformanceAerodynamicsAerospace SciencesAstrodynamicsAstronauticsAttitude ControlFlight DynamicsFlight MechanicsLaunch VehiclesSlip (Aerodynamics)Space Launch SystemsSpace SystemsSpace Systems and VehiclesSpacecraft Attitude Control KeywordsFlight Control DesignLaunch Vehicle DesignProportional Integral DerivativeAttitude Control SystemThrust Vector ControlAerodynamic ForceRoll ControlCenter of PressureAngle of AttackGraphical User InterfaceDigital Topics Guidance, Navigation, and Control