CLOS GUIDANCE FOR BANK TO TURN MISSILE
محتوى المقالة الرئيسي
الملخص
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.
تفاصيل المقالة
كيفية الاقتباس
تواريخ المنشور
المراجع
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