This thesis deals with a new type of launchers that are known under the name space planes. Due to the alternative mission profile and the strongly varying flight environment as compared with conventional aircraft and conventional launch vehicles, a major field of interest is flight mechanics and the simulation thereof in the design phase of such a vehicle, which is the main topic of the current study. Moreover, it is the intention to develop a generic model which allows for a fast analysis of flight mechanics of space vehicles.
Aerospace-Plane Flight Dynamics. Analysis of Guidance and Control Concepts
1998
324 pages
Report
Keine Angabe
Englisch
Test Facilities & Equipment , Aeronautics , Aerospaceplanes , Control systems , Performance evaluation , Flight simulation , Aerospace craft , Flight control , Guidance , Reentry vehicles , Space flight , Verification , Validation , Reentry simulation , Theses , Foreign technology , START tool , Flight mechanics , Guidance and control systems
British Aerospace Regional Jetliner Digital Flight Guidance Certification
British Library Conference Proceedings | 1992
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