Roll Control of Aeroballistic Flying Vehicles

A principle of creation of the high-precision guidance system based on a bundle, which consists of uncontrolled jet missile and controlling refit module, stabilized in roll is considered. The attitude control system provides the roll stabilization depending on data entering from the self-guidance head. Methods of analysis of images obtained from the self-guidance head are suggested as well as algorithms of calculation of roll parameters of the controlling refit module at various legs of the flight trajectory of the flying vehicle. A procedure of synthesis of the attitude control system is presented. Results of investigation of operation of the attitude control system are given.