Robust state dependent riccati equation based guidance laws

Proceedings of the American Control Conference

Volumn 5, Issue , 2001, Pages 3352-3357

  Balakrishnan, S N ^a   Xin, M ^a  

^a MISSOURI UNIVERSITY OF SCIENCE AND TECHNOLOGY   (United States)

Author keywords

Missile guidance law; Optimal control; Robust control; SDRE

Indexed keywords

ASYMPTOTIC STABILITY; CONTROL SYSTEM SYNTHESIS; EQUATIONS OF MOTION; ESTIMATION; FEEDBACK CONTROL; GEOMETRY; MATRIX ALGEBRA; NEURAL NETWORKS; NONLINEAR CONTROL SYSTEMS; PROBLEM SOLVING; RICCATI EQUATIONS; ROBUSTNESS (CONTROL SYSTEMS);

POLAR COORDINATES; STATE DEPENDENT COEFFICIENT; STATE DEPENDENT RICCATI EQUATION;

ELECTRONIC GUIDANCE SYSTEMS;

EID: 0034848820     PISSN: 07431619     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1109/acc.2001.946146     Document Type: Conference Paper

References (7)

1. Tactical and strategic missile guidance
2. Simple guidance law against highly maneuvering targets
3. ∞ robust guidance law for homing missiles
4. ∞ control via the state-dependent riccati equation technique
5. Neural networks for controller systems, a survey
6. Adaptive critic based neural networks for aircraft optimal control
7. Robust adaptive control using single-hidden-layer feedforward neural networks