Accession Number : AD0609225
Title : A METHOD OF ANALYSIS FOR THE DODCO OPTIMAL CONTROLLER.
Descriptive Note : Final rept. for Sep 62-Jun 64,
Corporate Author : AIR FORCE FLIGHT DYNAMICS LAB WRIGHT-PATTERSON AFB OHIO
Personal Author(s) : George,Frank L. ; Anderson,Ronald O.
Report Date : JUL 1964
Pagination or Media Count : 69
Abstract : An approximate representation of the DODCO Optimum Limited Information Adaptive Controller (DOLIAC) is formulated by a describing function approach. The describing function approximation of the DODCO controller coupled with conventional servo-analysis techniques is found to give reasonably accurate estimates of the stability characteristics of such systems. Results are verified by application to a specific plant and by digital computer simulation of the resulting system. (Author)
Descriptors : (*FLIGHT CONTROL SYSTEMS, FUNCTIONAL ANALYSIS), (*ADAPTIVE CONTROL SYSTEMS, FUNCTIONAL ANALYSIS), (*FUNCTIONAL ANALYSIS, ADAPTIVE CONTROL SYSTEMS), SYSTEMS ENGINEERING, OPTIMIZATION, COMPUTER LOGIC, NONLINEAR SYSTEMS, DIGITAL COMPUTERS, STABILIZATION SYSTEMS, FOURIER ANALYSIS, COMPLEX VARIABLES, ERRORS, CORRECTIONS, GAIN, SIMULATORS, CONTROL SYSTEMS
Distribution Statement : APPROVED FOR PUBLIC RELEASE