A backstepping design for flight path angle control

Proceedings of the IEEE Conference on Decision and Control

Volumn 4, Issue , 2000, Pages 3570-3575

  Harkegard O ^a   Glad, S T ^a  

^a LINKÖPING UNIVERSITY   (Sweden)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; COMPUTER SIMULATION; DIFFERENTIAL EQUATIONS; FEEDBACK; FLIGHT DYNAMICS; LIFT; LINEARIZATION; MATHEMATICAL MODELS; NONLINEAR CONTROL SYSTEMS; PARAMETER ESTIMATION; SYSTEM STABILITY;

BACKSTEPPING DESIGN; FEEDBACK LINEARIZATION; FLIGHT PATH ANGLE CONTROL; GLOBAL STABILIZING CONTROL;

CONTROL SYSTEM SYNTHESIS;

EID: 0034438580     PISSN: 01912216     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (10)

1. Linearization by output injection and nonlinear observers
2. Lean backstepping design for a jet engine compressor model
3. Flight control design using non-linear inverse dynamics
4. Linear quadratic design and μ-analysis of a fighter stability augmentation system