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Flight test experience and controlled impact of a remotely piloted jet transport aircraftThe Dryden Flight Research Center Facility of NASA Ames Research Center (Ames-Dryden) and the FAA conducted the controlled impact demonstration (CID) program using a large, four-engine, remotely piloted jet transport airplane. Closed-loop primary flight was controlled through the existing onboard PB-20D autopilot which had been modified for the CID program. Uplink commands were sent from a ground-based cockpit and digital computer in conjunction with an up-down telemetry link. These uplink commands were received aboard the airplane and transferred through uplink interface systems to the modified PB-20D autopilot. Both proportional and discrete commands were produced by the ground system. Prior to flight tests, extensive simulation was conducted during the development of ground-based digital control laws. The control laws included primary control, secondary control, and racetrack and final approach guidance. Extensive ground checks were performed on all remotely piloted systems; however, piloted flight tests were the primary method and validation of control law concepts developed from simulation. The design, development, and flight testing of control laws and systems required to accomplish the remotely piloted mission are discussed.
Document ID
19890006539
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Horton, Timothy W.
(NASA Hugh L. Dryden Flight Research Facility Edwards, CA, United States)
Kempel, Robert W.
(NASA Hugh L. Dryden Flight Research Facility Edwards, CA, United States)
Date Acquired
September 5, 2013
Publication Date
November 1, 1988
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
H-1447
NASA-TM-4084
NAS 1.15:4084
Accession Number
89N15910
Funding Number(s)
PROJECT: RTOP 505-44-24
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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