MODERN MISSILE FLIGHT CONTROL DESIGN: AN OVERVIEW

摘要

The requirement of high agility in the entire flight envelope will dominate the flight control design for future missile systems. The desin requirements for the next-generation autopilots will include not fast response to the required acceleration demands and extreme maneuvarability while maintaining stability, but also robustness over a wide range of mission profiles at all altitudes. An overview of different control techniques for missile autopilot design is presented in this paper.