Integrated missile guidance and control: A state dependent Riccati differential equation approach

IEEE Conference on Control Applications - Proceedings

Volumn 1, Issue , 1999, Pages 243-248

  Palumbo, Neil F ^a   Jackson, Todd D ^a  

^a JOHNS HOPKINS UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

APPROXIMATION THEORY; COMPUTER SIMULATION; CONTROL SYSTEM SYNTHESIS; DEGREES OF FREEDOM (MECHANICS); INTEGRATED CONTROL; MISSILES; MONTE CARLO METHODS; OPTIMIZATION; RICCATI EQUATIONS;

TACTICAL BALLISTIC MISSILE (TBM);

ELECTRONIC GUIDANCE SYSTEMS;

EID: 0033335428     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (12)