H∞ parameter identification for inflight detection of aircraft icing: The time-varying case

Control Engineering Practice

Volumn 9, Issue 12, 2001, Pages 1327-1335

  Melody, James W ^a   Hillbrand, Thomas ^b   Başar, Tamer ^a   Perkins, William R ^a  

^a University of Illinois at Urbana Champaign   (United States)

^b DARMSTADT UNIVERSITY OF TECHNOLOGY   (Germany)

Author keywords

Aircraft control; H infinity; Identification; Robustness; Time varying systems

Indexed keywords

AIRCRAFT; ALGORITHMS; COMPUTER SIMULATION; FLIGHT DYNAMICS; ICE CONTROL; IDENTIFICATION (CONTROL SYSTEMS); TURBULENCE;

AIRCRAFT ICING; NOISY STATE MEASUREMENTS;

TIME VARYING CONTROL SYSTEMS;

AIRCRAFT; CONTROL SYSTEM; DETECTION METHOD; ICING;

EID: 0035678273     PISSN: 09670661     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0967-0661(01)00081-8     Document Type: Article

References (13)

1. Aircraft aerodynamic effects due to large droplet ice accretions
2. Effect of ice accretion on aircraft flight dynamics
3. An interdisciplinary approach to inflight aircraft icing safety
4. Statistical study of aircraft icing accidents
5. ∞ methods
6. Parameter identification for inflight detection of aircraft icing
7. Sensor integration for inflight icing characterization using neural networks
8. Icing effects on aircraft stability and control determined from flight data
9. NASA/FAA tailplane icing program overview
10. Detection and classification of aircraft icing using neural networks