Based On Dynamic Pressure Selected Parameters Of The Spacecraft Attitude Control System Design

This article describes a remote controlled vehicle has, with quick, powerful, longer range, the use of simple, easy maintenance and low cost. As a high-precision guided missiles and intermediate-range missiles a weapon between, this article describes a remote control aircraft in both domestic and international market, high demand military trade, which led to vigorously promote the domestic research unit weapons system for the weapon. Accuracy weapons of modern warfare combat increasingly high demand, in improving the fight against the exact same time to consider lowering production costs, the installation of conventional aircraft guidance device to improve the precision attack aircraft. Adopt comprehensive measures to improve the fire intensity; using the new shell material, to reduce weight; using high-energy propellants and high explosives or other high power of the filler; with a variety of roles in the fuzzed and warhead in order to further increase the range and improve and expand the use of power. First introduced the development status of certain domestic and foreign aircraft, and spacecraft attitude control system design of the study, including aircraft frequency domain design, mathematical simulation, semi-physical simulation, etc., while the attitude control system design of some key technology Looking attitude control design future trends.