Global configuration stabilization for the VTOL aircraft with strong input coupling

Proceedings of the IEEE Conference on Decision and Control

Volumn 4, Issue , 2000, Pages 3588-3589

  Olfati Saber, R ^a  

^a MASSACHUSETTS INSTITUTE OF TECHNOLOGY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT LANDING; ASYMPTOTIC STABILITY; CLOSED LOOP CONTROL SYSTEMS; COMPUTER SIMULATION; FLIGHT DYNAMICS; STATE FEEDBACK; VTOL/STOL AIRCRAFT;

EXPONENTIAL STABILITY; GLOBAL CONFIGURATION STABILIZATION; STRONG INPUT COUPLING; TRAJECTORY TRACKING;

CONTROL SYSTEM SYNTHESIS;

EID: 0034438553     PISSN: 01912216     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (6)

1. Nonlinear control design for slightly non-minimum phase systems
2. A different look at output tracking: Control of a VTOL aircraft
3. Cascade normal forms for underactuated mechanical systems
4. Controller design for a class of underactuated nonlinear systems
5. Smooth stabilization implies co-prime factorization