No AccessOutput Tracking of Non-Minimum Phase DynamicsAnshu Siddarth and John ValasekAnshu SiddarthTexas A&M UniversitySearch for more papers by this author and John ValasekTexas A&M UniversitySearch for more papers by this authorPublished Online:14 Jun 2012https://doi.org/10.2514/6.2011-6487SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About Previous chapter Next chapter FiguresReferencesRelatedDetailsSee PDF for referencesCited byTwo time‐scale assignment with state extension for an autonomous helicopter27 February 2020 | Asian Journal of Control, Vol. 23, No. 4A modular adaptive control design with ISS analysis for nonminimum phase hypersonic vehicle models25 March 2018 | International Journal of Adaptive Control and Signal Processing, Vol. 32, No. 6Feedback Control of a Nonlinear Non-Minimum Phase Missile with Limited Modeling InformationAnshu Narang-Siddarth, Florian Peter and Florian Holzapfel2 January 2015Tracking Control for a Non-Minimum Phase Autonomous HelicopterAnshu Siddarth and John Valasek6 September 2012 What's Popular AIAA Guidance, Navigation, and Control Conference 08 August 2011 - 11 August 2011Portland, Oregonhttps://doi.org/10.2514/6.2011-6487 Crossmark TopicsAircraft ControlAircraft Flight Control SystemAircraft OperationsAircraft Operations and TechnologyAircraft Stability and ControlAircraftsControl TheoryFeedback ControlFlight TrainingFlying QualitiesGuidance, Navigation, and Control SystemsNonlinear Control TheoryTakeoff and LandingVertical Takeoff and Landing KeywordsProportional ControlNonlinear SystemsControl DerivativesFeedback LinearizationAngle of AttackSingular PerturbationTake off and LandingControl AlgorithmDouglas DC 8Vertical Take off and LandingPDF Topics Guidance, Navigation, and Control