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Aircraft digital control design methodsInvestigations were conducted in two main areas: the first area is control system design, and the goals were to define the limits of 'digitized S-Plane design techniques' vs. sample rate, to show the results of a 'direct digital design technique', and to compare the two methods; the second area was to evaluate the roughness of autopilot designs parametrically versus sample rate. Goals of the first area were addressed by (1) an analysis of a 2nd order example using both design methods, (2) a linear analysis of the complete 737 aircraft with an autoland obtained using the digitized S-plane technique, (3) linear analysis of a high frequency 737 approximation with the autoland from a direct digital design technique, and (4) development of a simulation for evaluation of the autopilots with disturbances and nonlinearities included. Roughness evaluation was studied by defining an experiment to be carried out on the Langley motion simulator and coordinated with analysis at Stanford.
Document ID
19750022116
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Tashker, M. G.
(Stanford Research Inst. Menlo Park, CA, United States)
Powell, J. D.
(Stanford Univ.)
Date Acquired
September 3, 2013
Publication Date
June 1, 1975
Subject Category
Aircraft Stability And Control
Report/Patent Number
MPR-6
NASA-CR-143321
Report Number: MPR-6
Report Number: NASA-CR-143321
Accession Number
75N30189
Funding Number(s)
CONTRACT_GRANT: NSG-1137
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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