|
Volumn , Issue , 2001, Pages 1512-1517
|
Computation of the zero error manifold for a problem of smooth vertical landing of an helicopter
|
Author keywords
Aerospace Systems; Non linear Oscillations; Output Regulation; Trajectory Tracking in Non linear Systems
|
Indexed keywords
CONTROL ENGINEERING;
AEROSPACE SYSTEMS;
APPROXIMATED SOLUTIONS;
NONLINEAR OSCILLATION;
OSCILLATING PLATFORM;
OUTPUT REGULATION;
REGULATOR EQUATIONS;
STEADY STATE SOLUTION;
VERTICAL OSCILLATIONS;
LINEAR SYSTEMS;
|
EID: 84947474939
PISSN: None
EISSN: None
Source Type: Conference Proceeding
DOI: 10.23919/ecc.2001.7076133 Document Type: Conference Paper |
Times cited : (3)
|
References (6)
|