The problem of guiding an instrumented aircraft to follow a pre-assigned trajectory using the Portable Automatic Calibration Tracker (PACT) data is considered in this paper. Guidance control is formulated as an optimal linear state regulator problem for a discrete time-delayed system. Responses to some flight courses of interest have, been achieved through computer system simulation. Post-flight test data obtained from the PACT confirm the basic validity of the theoretical results.
Automatic Flight Guidance Using the Portable Automatic Calibration Tracker Data
IEEE Transactions on Aerospace and Electronic Systems ; AES-11 , 6 ; 1377-1383
1975-11-01
937316 byte
Article (Journal)
Electronic Resource
English
Automatic flight guidance using the portable automatic calibration tracker data
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