Analysis of two-channel control according to the proportional navigation method

Abstract

In this paper the equations of the ideal constraints of the proportional navigation method have been presented, as well as the simplified equations applicable in two-channel anti-aircraft missile control.Using the elaborated mathematical model of homing the test missile some numerical experiments have been conducted, regarding the influence of the undertaken simplification in realisation of the homing method constrains on the flight dynamics and the hit accuracy of the canard configuration rocket.