The problem of precision missile guidance: LQR and H∞ control frameworks

Proceedings of the IEEE Conference on Decision and Control

Volumn 2, Issue , 2001, Pages 1535-1540

  Savkin, Andrey V ^a   Pathirana, Pubudu N ^a   Faruqi, Farhan A ^a  

^a UNIVERSITY OF NEW SOUTH WALES   (Australia)

Author keywords

H control; Optimal control; Precision missile guidance; Robust control

Indexed keywords

AEROSPACE ENGINEERING; DIFFERENTIAL EQUATIONS; FEEDBACK CONTROL; KINEMATICS; OPTIMAL CONTROL SYSTEMS; ROBUSTNESS (CONTROL SYSTEMS); THEOREM PROVING; VECTORS;

PRECISION MISSILE GUIDANCE;

ELECTRONIC GUIDANCE SYSTEMS;

EID: 0035712720     PISSN: 01912216     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (9)

1. ∞ control and the absolute stabilizability of uncertain systems
2. Nonlinear versus linear control in the absolute stabilizability of uncertain linear systems with structured uncertainty
3. Minimax optimal control of uncertain systems with structured uncertainty
4. Robust control with a terminal state constraint
5. Feedback and optimal sensitivity: Model reference transformations, multiplicative seminorms, and approximate inverses
6. ∞ control with transients