Title :
Autopilot designs for BTT CLOS guidance
Author :
Teoh, E.K. ; Mital, D.P. ; Ang, K.S.
Author_Institution :
Sch. of Electr. & Electron. Eng., Nanyang Technol. Inst., Singapore
Abstract :
Optimum autopilot designs are presented for bank-to-turn CLOS (BTT) guidance. BTT is capable of producing higher lift-to-drag ratio. A linear quadratic optimal technique is used for the design of the roll and pitch autopilot. Simulation results have demonstrated the improvements in control with the linear quadratic optimal design
Keywords :
aerospace simulation; aircraft control; aircraft instrumentation; military systems; missiles; optimal control; bank-to-turn CLOS; command to line of sight; guidance; lift-to-drag ratio; linear quadratic optimal design; manoeuvre; roll and pitch autopilot; simulation; Acceleration; Aerospace control; Aircraft; Banking; Control systems; Design engineering; Elevators; Missiles; Optimal control; Servomechanisms;
Conference_Titel :
Circuits and Systems, 1991., IEEE International Sympoisum on
Print_ISBN :
0-7803-0050-5
DOI :
10.1109/ISCAS.1991.176107
