1996 · 22 citations · 1 references
EngineeringAerospace EngineeringSystems EngineeringFlight DynamicsFlight MechanicsVehicle DynamicsAttitude ControlManeuveringManeuvering ControlMotion ControlVehicle ControlVehicle Control SystemsControl System ModelingFlight Path ControlFlight Path PerturbationsIntegrated GuidanceLateral ControlLateral Motion ControlNavigation Guidance SystemsProportional Navigation
This paper describes the design of a movingmass, trim-control system for maneuvering antisymmetric reentry vehicles. The moving-mass trim controller is composed of three equal masses that are independently positioned in order to deliver a desired center of mass position. For a slowly spinning reentry vehicle, the mass offset creates a trim angle-of-at tack to generate modest flight path corrections. A proportional navigation guidance scheme is used to determine the desired lateral accelerations required to hit the target. Mass movements are calculated from the desired lateral accelerations. Simulation results for the integrated guidance and control system are presented for a typical reentry vehicle.
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