Title :
"No-escape" firing envelopes revisited
Author :
Shinar, Josef ; Tabak, Russel
Author_Institution :
Fac. of Aerosp. Eng., Technion-Israel Inst. of Technol., Haifa, Israel
fDate :
29 June-1 July 1994
Abstract :
The effect of the lethal range of a coasting guided missile on the optimal missile avoidance strategy of a constant speed aircraft is investigated in the horizontal plane. The guidance law of the missile is proportional navigation and it assumed to have first-order dynamics. A great sensitivity of the "no-escape" firing envelope to the values of the time constant and lethal range of the missile is observed.
Keywords :
missile guidance; navigation; optimal control; proportional control; coasting guided missile; firing envelopes; first-order dynamics; lethal range; missile avoidance strategy; no-escape firing envelopes; proportional navigation; Aerodynamics; Aerospace engineering; Aircraft navigation; Aircraft propulsion; Missiles; Modems; Transfer functions; Turning; Vehicle dynamics; Vehicles;
Conference_Titel :
American Control Conference, 1994
Print_ISBN :
0-7803-1783-1
DOI :
10.1109/ACC.1994.751904
