Accession Number : ADA166596
Title : Vectored Thrust Digital Flight Control for Crew Escape. Volume 2.
Descriptive Note : Final rept. 1 Jun 82-28 Feb 85,
Corporate Author : SCIENTIFIC SYSTEMS INC CAMBRIDGE MA
Personal Author(s) : Carroll,James V ; Gendron,Robert F
Report Date : Dec 1985
Pagination or Media Count : 208
Abstract : Work of Meyer and Cicolani was adapted for application to open seat escape systems in current Air Force fighter aircraft. The control system design is a fully self-contained system whose major on-seat components are: acceleration, rate, attitude and altitude sensors, real-time control logic imbedded on a microprocessor chip, rocket thrusters with thrust vectoring and throttling capability, and various avionics and support subsystem hardware items (e.g., power supply). The control concept is based on a comparison of measured translational and rotational accelerations with desired values; the propulsion system is then configured to provide adequate energy to follow the desired trajectory and simultaneously eliminate acceleration errors. The concept uses nonlinear models and incorporates state and control constraints. Volume I (AD-A166580) contains the detailed documentation of specification development, control logic design, hardware identification, and trade study efforts. Volume II contains a description of the prototype design, real time breadboard simulation, and the results and analysis of the verification task. Keywords: Modern control theory, Model algorithmic control, Acceleration control, Ejection seat control.
Descriptors : *EJECTION SEATS , *THRUST VECTOR CONTROL SYSTEMS , MATHEMATICAL MODELS , ALGORITHMS , AVIONICS , CONTROL , SIMULATION , THROTTLING , FIGHTER AIRCRAFT , DIGITAL SYSTEMS , CONTROL SYSTEMS , ATTITUDE CONTROL SYSTEMS , DETECTORS , FLIGHT CONTROL SYSTEMS , FLIGHT CREWS , MICROPROCESSORS , REAL TIME , ACCELERATION , PROTOTYPES , PROPULSION SYSTEMS , NONLINEAR SYSTEMS , SELF CONTAINED , CREWS , ERRORS , BREADBOARD MODELS , POWER SUPPLIES , JET FIGHTERS , CONTROL THEORY , ALTITUDE , ESCAPE SYSTEMS , ROTATION , TRAJECTORIES , AIR FORCE EQUIPMENT , ROCKETS , CONTROL SEQUENCES
Subject Categories : Flight Control and Instrumentation
Escape, Rescue and Survival
Distribution Statement : APPROVED FOR PUBLIC RELEASE