Accession Number : AD0875087
Title : Effects of Data Rate and Time Constants on a Glide Missile Using Bang-Bang and Continuous Controllers.
Descriptive Note : Master's thesis,
Corporate Author : AIR FORCE INST OF TECH WRIGHT-PATTERSON AFB OH SCHOOL OF ENGINEERING
Personal Author(s) : Garnto, Ira W.
Report Date : MAR 1970
Pagination or Media Count : 92
Abstract : A computer study was made of the affects of guidance data rate and control response time on the accuracy at the target of a controlled bomb. A single guidance system was used, but two control systems were employed, a bang-bang and a continuous system. For the bang-bang system, maximum allowable data rate and control response are one and two seconds, respectively. Inside these limits, no predictable pattern can be established, and each combination must be evaluated. The continuous system provides very good patterns that are highly predictable. Error increases with increases in both data rate and response time. (Author)
Descriptors : (*BOMB TRAJECTORIES, MATHEMATICAL MODELS), (*GUIDED BOMBS, COMMAND GUIDANCE), STABILIZATION SYSTEMS, YAW, ANGLE OF ATTACK, MISS DISTANCE, EQUATIONS OF MOTION, EULER ANGLES, AERODYNAMIC CHARACTERISTICS, COMPUTER PROGRAMS, THESES.
Subject Categories : Computer Programming and Software
Distribution Statement : APPROVED FOR PUBLIC RELEASE