A proposed manned spacecraft design, designated the HL-20, has been under investigation at Langley Research Center. Included in that investigation are flight control design and flying qualities studies utilizing a man-in-the-loop real-time simulator. This report documents the current real-time simulation model of the HL-20 lifting body vehicle, known as version 2.0, presently in use at NASA Langley Research Center. Included are data on vehicle aerodynamics, inertias, geometries, guidance and control laws, and cockpit displays and controllers. In addition, trim case and dynamic check case data is provided. The intent of this document is to provide the reader with sufficient information to develop and validate an equivalent simulation of the HL-20 for use in real-time or analytical studies.
Real-Time Simulation Model of the HL-20 Lifting Body
1992
423 pages
Report
Keine Angabe
Englisch
Space Launch Vehicles & Support Equipment , Computerized simulation , Control theory , Flight characteristics , Flight control , Lifting bodies , Real time operation , Spacecraft design , Manned spacecraft , Aerodynamics , Cockpit simulators , Computer programs , Display devices , Flight simulators , Mathematical models
Real-time simulation model of the HL-20 lifting body
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