Title :
An implementable high-order guidance law for homing missiles
Author :
Aggarwal, Romesh ; Boudreau, Daniel
Author_Institution :
Raytheon Electron. Syst., Raytheon Co., Tewksbury, MA, USA
Abstract :
A high-order optimal guidance law for tactical missiles is derived using measurable/realizable states in its autopilot/airframe (AP/AF) plant model. This derivation yields a form of the guidance law that can be implemented in an operational missile system
Keywords :
missile guidance; optimal control; transfer functions; autopilot/airframe plant model; high-order guidance law; homing missiles; measurable/realizable states; tactical missiles; Acceleration; Accelerometers; Aerodynamics; Geometry; Missiles; Navigation; Optimal control; Stability; State-space methods; Transfer functions;
Conference_Titel :
Decision and Control, 1995., Proceedings of the 34th IEEE Conference on
Conference_Location :
New Orleans, LA
Print_ISBN :
0-7803-2685-7
DOI :
10.1109/CDC.1995.480614
