This content is not included in
your SAE MOBILUS subscription, or you are not logged in.
The Influence of Piloted Flight Simulator Studies on the Design of the SST Instruments
Annotation ability available
Sector:
Language:
English
Abstract
For the Boeing SST, flight simulators are providing important insight into problems of stability, control, and flight information display in advance of the actual cutting of metal for flying hardware. Simulator investigations have yielded tentative solutions to several flight instrumentation problems: the optimum scale factor for the pilot's pitch indicator; the economical evaluation of experimental landing displays through the use of CRT line-writing techniques; and the development of a display system for informing the pilot of his situation with respect to a prescribed sonic-boom-limited climb or descent profile.
Authors
Citation
Annin, G., "The Influence of Piloted Flight Simulator Studies on the Design of the SST Instruments," SAE Technical Paper 670306, 1967, https://doi.org/10.4271/670306.Also In
References
- Brockway B. W. Tubb D. G. “Development and Application of the Boeing Space-Flight Simulator.” Paper presented at AIAA Guidance and Control Conference Seattle Aug. 15 1966
- Noxon P. A. “Microvision Heads-Up Displays: Fog Simulation and Measurement.” The Bendix Corp. Oct. 28 1966
- Turcat A. “The Pilot and All-Weather Landing.” 15th Technical Conference Lucerne, Switzerland April 1963
- Annin G. D. Hansen R. “Flying the Sonic Boom Profile.” Working Paper 96, IATA Conference 16 April 1965