Journal of Theoretical
and Applied Mechanics

33, 4, pp. 899-908, Warsaw 1995

Simulation of the anti-aircraft, long-range missile guidance

Józef Gacek, Bogdan Machowski
A mathematical model of the missile guidance system in terms of the ''three point'' and the ''half-to-half lead guidance law'' methods, respectively, has been presented in the paper. A hypothetical anti-aircraft, long-range missile (a-a missile) and the target motion hypothesis have been assumed.