Print Email Facebook Twitter A Variable Stability In-Flight Simulation System using Incremental Non-Linear Dynamic Inversion Title A Variable Stability In-Flight Simulation System using Incremental Non-Linear Dynamic Inversion Author Scholten, Pepijn (TU Delft Aerospace Engineering) Contributor van Paassen, M.M. (mentor) Mulder, Max (mentor) Degree granting institution Delft University of Technology Programme Aerospace Engineering Date 2019-01-24 Subject VariableStabilityIn-FlightSimulationHandlingQualitiesIncrementalNon-linearDynamicInversion To reference this document use: http://resolver.tudelft.nl/uuid:fbdfb1fe-b5a9-46b4-841c-27e4268a2925 Embargo date 2020-01-17 Part of collection Student theses Document type master thesis Rights © 2019 Pepijn Scholten Files PDF Final_Thesis_Pepijn_Schol ... Online.pdf 30.15 MB Close viewer /islandora/object/uuid:fbdfb1fe-b5a9-46b4-841c-27e4268a2925/datastream/OBJ/view