CLOS GUIDANCE FOR BANK TO TURN MISSILE

Main Article Content

Mohammed.Z. Al-Faiz
Yousif.L Al-Mashhidina

Abstract

Bank to turn (BTT) control is used to implement a command - to line of- sight (CLOS) guidance law. Physical description of the prineiples involved is given and a 10.th order nonlincar deterministic model proposed. Conventional control is used to design a closed loop controller for the nonlinear system


Continuous system simulation techniques are employed to explain the effect of bank turn on cross coupling of yaw, pitch and roll channels. Detailed simulation studies are then used for a wide range of engagement sinearieous for trajectory of Missile/ Target interception. The target model is considered for three cases: stationary, moving and maneuvering targets. Satisfactory results are bbtained for capturing the targets.

Article Details

Section

Articles

How to Cite

“CLOS GUIDANCE FOR BANK TO TURN MISSILE” (2005) Journal of Engineering, 11(03), pp. 441–453. doi:10.31026/j.eng.2005.03.01.

References

Ching. F.L and Szu P.L (1984), Robust missile autopliot design using a generalized singular optimal control technique, Journal Guidance. Control & Dynamies vol.8.No.4.

Garnell, P,(1980). Guided weapam eantrol systent. 2nd eelition Perggmon Ps Osfond

Hussain, HA. (1995), Optimal response of autopilot for BTT missile, M.Sc. Thesis.MEC, Baghdad

Control &Guidance Eng. Dept

Jack. N.Nielsen (1960): Missile acrodynamics, first edition NewYork

Lightbody. G. & Irwin. G.W. (1995), Direct ncural model reference adaptive control, IEE Proc

Control Theory Appl. Vol. 142, No.1 TANUARY.

Matlab for windows ver.5.1 July. (1997), programming language.

Majeed. S A (1996), Design of autopilot by linear quadratic regulator. M.Sc. Thesis MEC Baghdad, A/C Amement Enp Dept..

Rasheed. A. (1996). Design & analysis of discrete loppituslinal autopilot for BIL missile. M.Se Thesis. MHC,Baghdad „A/C Armemnen Fa Dept

Roddy, D. J, and. Irwin, G. Wand Wilson. H. (1984). Optimal controllers for bank- to-turn CLOS guidance, IE Proc, vol. 131. No. 4 JULY PP 109.116

Roddy, D. J, and, Irwin, G. W. (1983), Application of modern control to bank To-tun guidance using digital simulation, Proc.summer computer simulation conference Vancouver, Canada July (North-Holland publ. (0) vol. 1- pp. 296 301

an Y.M and Borrie JA (1984). Missile guidance based on kalman filter estimation of target nancuver, TEEF Trns. On Aerospace and electronic system vol. 20-No 6november

Williams D and Friedland B (1987) Modern control theory for design of autopilots for bank totum missile" Journal Cuidance Control & Dypamnies Vol 10. NO 4,.pp 378-386