Title :
The STOL Maneuver Technology Demonstrator manned simulation test program
Author :
Feeser, Kenneth A. ; Zeh, James M. ; Leggett, David B.
Author_Institution :
Wright Res. Dev. Center, Wright-Patterson AFB, OH, USA
Abstract :
A description is given of the STOL (short takeoff and landing) Maneuver Technology Demonstrator (S/MTD) simulation, a high-fidelity pilot-in-the-loop motion base simulation. The simulation was used to evaluate takeoff, landing, and air-to-air tasks before first flight of the S/MTD aircraft to improve aircraft flying qualities, conduct engineering research, and insure safety of flight. 208 hours of pilot-in-the-loop evaluations were conducted. The authors describe the simulation hardware, test approach/results of the pilot vehicle interface (PVI), and flying qualities and aircraft failure evaluations in the STOL landing (SLAND) flight control system mode
Keywords :
aerospace computing; aerospace simulation; aircraft control; S/MTD aircraft; STOL Maneuver Technology Demonstrator; aerospace computing; aerospace simulation; air-to-air tasks; aircraft failure; flight control; landing; pilot vehicle interface; pilot-in-the-loop motion base simulation; safety; short takeoff and landing; takeoff; Aerospace control; Aerospace engineering; Aerospace safety; Aerospace simulation; Air safety; Aircraft propulsion; Automotive engineering; Hardware; System testing; Vehicles;
Conference_Titel :
Aerospace and Electronics Conference, 1989. NAECON 1989., Proceedings of the IEEE 1989 National
Conference_Location :
Dayton, OH
DOI :
10.1109/NAECON.1989.40240