A velocity-based framework for the robust stability analysis of dynamic inversion flight controllers

Proceedings of the American Control Conference

Volumn 5, Issue , 2001, Pages 3341-3345

  Tsourdos, A ^a   Leith, D J ^b   Leithead, W E ^b   White, B A ^a  

^a CRANFIELD UNIVERSITY   (United Kingdom)

^b UNIVERSITY OF STRATHCLYDE   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; FLIGHT DYNAMICS; LINEARIZATION; ROBUSTNESS (CONTROL SYSTEMS); SYSTEM STABILITY; VEHICLES; VELOCITY CONTROL;

DYNAMIC INVERSION FLIGHT CONTROLLER; PARAMETRIC UNCERTAINTY;

NONLINEAR CONTROL SYSTEMS;

EID: 0034842160     PISSN: 07431619     EISSN: None     Source Type: Journal    
DOI: 10.1109/ACC.2001.946144     Document Type: Article

References (6)

1. A study of autopilots for the adaptive control of tactical guided missiles
2. Gain-scheduled & nonlinear & systems: Dynamic analysis by velocity-based linearisation families
3. Input-output linearisation by velocity-based gain-scheduling
4. Robust nonlinear design of a high incidence missile autopilot