A real-time dynamic model of the propulsion system for a Short Take-Off and Vertical Landing (STOVL) aircraft was developed for the AD100 simulation environment. The dynamic model was adapted from a FORTRAN based simulation using the dynamic programming capabilities of the AD100 ADSIM simulation language. The dynamic model includes an aerothermal representation of a turbofan jet engine, actuator and sensor models, and a multivariable control system. The AD100 model was tested for agreement with the FORTRAN model and real-time execution performance. The propulsion system model was also linked to an airframe dynamic model to provide an overall STOVL aircraft simulation for the purposes of integrated flight and propulsion control studies. An evaluation of the AD100 system for use as an aircraft simulation environment is included.
AD100 Implementation of a Real-Time Stovl Aircraft Propulsion System
1990
20 pages
Report
No indication
English
Propulsion optimization for conceptual STOVL aircraft
AIAA | 1989
|STOVL Propulsion System Selections Effect on Aircraft Design
British Library Conference Proceedings | 1997
|Integrated propulsion system requirements for control of STOVL aircraft
Tema Archive | 1990
|