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Rotary-wing aircraft terrain-following/terrain-avoidance system developmentWork being accomplished to develop a real-time, piloted simulation of a helicopter using the vertical motion simulator at NASA Ames is discussed. The trajectory generation algorithm and the flight path controller are described, and the software integration of the entire terrain following/terrain avoidance (TF/TA) system is discussed. Real-time simulation requirements and the unique features of applying TF/TA system to helicopter flight are summarized. Initial results indicate that the system is satisfactory for automatic, low level TF/TA helicopter flight.
Document ID
19860062718
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Dorr, D. W.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1986
Subject Category
Aircraft Stability And Control
Report/Patent Number
AIAA PAPER 86-2147
Report Number: AIAA PAPER 86-2147
Accession Number
86A47456
Distribution Limits
Public
Copyright
Other

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