Piloted Evaluation of an Integrated Methodology for Propulsion and Airframe Control Design
- Author
- Simon, Donald L.
- Published
- Sep 1, 1994.
- Physical Description
- 1 electronic document
- Additional Creators
- Bright, Michelle M., Garg, Sanjay, Mattern, Duane L., Ranaudo, Richard J., and Odonoghue, Dennis P.
Online Version
- hdl.handle.net , Connect to this object online.
- Restrictions on Access
- Unclassified, Unlimited, Publicly available.
Free-to-read Unrestricted online access - Summary
- An integrated methodology for propulsion and airframe control has been developed and evaluated for a Short Take-Off Vertical Landing (STOVL) aircraft using a fixed base flight simulator at NASA Lewis Research Center. For this evaluation the flight simulator is configured for transition flight using a STOVL aircraft model, a full nonlinear turbofan engine model, simulated cockpit and displays, and pilot effectors. The paper provides a brief description of the simulation models, the flight simulation environment, the displays and symbology, the integrated control design, and the piloted tasks used for control design evaluation. In the simulation, the pilots successfully completed typical transition phase tasks such as combined constant deceleration with flight path tracking, and constant acceleration wave-off maneuvers. The pilot comments of the integrated system performance and the display symbology are discussed and analyzed to identify potential areas of improvement.
- Other Subject(s)
- Collection
- NASA Technical Reports Server (NTRS) Collection.
- Note
- Document ID: 19950006350.
Accession ID: 95N12763.
NASA-TM-106741.
ARL-TR-519.
NAS 1.15:106741.
E-9149.
AD-A290207.
Guidance, Navigation and Control Conference; 1-3 Aug. 1994; Scottsdale, AZ; United States. - Terms of Use and Reproduction
- Copyright, Distribution as joint owner in the copyright.
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