Nonlinear attitude control laws for the Bell 412 helicopter

Journal of Guidance, Control, and Dynamics

Volumn 31, Issue 1, 2008, Pages 44-52

  Walker, Daniel J ^a,c   Voskuijl, Mark ^a,c   Manimala, Binoy J ^a,c   Gubbels, Arthur W ^b,d  

^a UNIVERSITY OF LIVERPOOL   (United Kingdom)

^b NATIONAL RESEARCH COUNCIL CANADA   (Canada)

^c Engineering Department

^d Institute of Aerospace Research

Author keywords

[No Author keywords available]

Indexed keywords

BANDWIDTH; CLOSED LOOP SYSTEMS; FEEDBACK CONTROL; HELICOPTERS; NONLINEAR CONTROL SYSTEMS;

NONCOMBAT MISSION; NONLINEAR ELEMENTS; PITCH AXIS PERFORMANCE;

ATTITUDE CONTROL;

EID: 43649084390     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/1.28945     Document Type: Article

References (21)