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Control logic to track the outputs of a command generator or randomly forced targetA procedure is presented for synthesizing time-invariant control logic to cause the outputs of a linear plant to track the outputs of an unforced (or randomly forced) linear dynamic system. The control logic uses feed-forward of the reference system state variables and feedback of the plant state variables. The feed-forward gains are obtained from the solution of a linear algebraic matrix equation of the Liapunov type. The feedback gains are the usual regulator gains, determined to stabilize (or augment the stability of) the plant, possibly including integral control. The method is applied here to the design of control logic for a second-order servomechanism to follow a linearly increasing (ramp) signal, an unstable third-order system with two controls to track two separate ramp signals, and a sixth-order system with two controls to track a constant signal and an exponentially decreasing signal (aircraft landing-flare or glide-slope-capture with constant velocity).
Document ID
19770059905
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Trankle, T. L.
(Systems Control, Inc. West Palm Beach, Fla., United States)
Bryson, A. E., Jr.
(Stanford University Stanford, Calif., United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1977
Subject Category
Aircraft Communications And Navigation
Report/Patent Number
AIAA PAPER 77-1041
Meeting Information
Meeting: Guidance and Control Conference
Location: Hollywood, FL
Start Date: August 8, 1977
End Date: August 10, 1977
Accession Number
77A42757
Funding Number(s)
CONTRACT_GRANT: NGL-05-020-007
Distribution Limits
Public
Copyright
Other

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