V/STOL aircrafts have different flight modes, including conventional mode, hover and transition flight. And the control effectors include thrust engines, thrust vectors and aerodynamic actuators. The dynamic model of V/STOL aircrafts varies significantly due to jet-induced effect during hover and transition flight. In this paper, dynamic model of V/STOL aircraft propulsion system and jet-induced forces are built. The 6-DOF nonlinear equations of motion, for a V/STOL UAV are formulated and simulated. Simulations results validate the dynamic model built in this paper. And the dynamic model could be used for propulsion system and control system design.
Dynamics modeling and analysis of thrust-vectored V/STOL aircraft
2013-07-01
360148 byte
Conference paper
Electronic Resource
English
Takeoff performance of jet-propelled conventional and vectored-thrust STOL aircraft
Engineering Index Backfile | 1968
|Multi-Mission V/STOL with Vectored Thrust Engines
NTIS | 1981
|Multi-mission V/STOL with vectored thrust engines
AIAA | 1981
|