GN&C Design and Analysis Branch, NASA Johnson Space Center 1 May 2000 – 1 May 2001 Total award $97,320 As opposed to traditional synthesis techniques, in which the nonlinear plant is separated into several linearized models at discrete operating points, and a closed-loop controller is synthesized for each one, Dynamic Inversion seeks to synthesize a … Continue reading Synthesis and Evaluation of Robust Dynamic Inversion Flight Controllers for X-38 Class Re-Entry Vehicles