This paper studies the conditions of the successful takeoff and climbing of the aerospace vehicle. By analyzing the longitudinal kinematics model and dynamic model of the vehicle, the take-off constraints determined by integrating with the lift-drag ratio, thrust-to-weight ratio, flight speed and take-off weight. Moreover, the algebraic form of the maximum take-off weight is also derived to ensure that the aircraft can successfully take off under a fixed configuration. Finally, the simulation results verify the effectiveness of the proposed methods.
Determination of take-off constraints for the aerospace vehicle
2018-08-01
255456 byte
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
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