Title :
Advanced Guidance Laws for Acceleration Constrained Missile, Randomly Maneuvering Target and Noisy Measurements
Author_Institution :
Drexel University, ECE Dept., Philadelphia, PA
Keywords :
Acceleration; Differential equations; Missiles; Noise measurement; Optimal control; State estimation; Stochastic processes; Stochastic resonance; Technological innovation; Vectors;
Conference_Titel :
Aerospace Control Systems, 1993. Proceedings. The First IEEE Regional Conference on
DOI :
10.1109/AEROCS.1993.721003
