|
|
Volumn 2, Issue 2, 2011, Pages 158-184
|
|
Aeroelastic analysis of remotely controlled research vehicles with numerous control surfaces
|
|
Author keywords
Actuators; Control systems; Modelling; Remote handling devices
|
|
Indexed keywords
AEROELASTIC ANALYSIS;
ARTIFICIAL CONTROL;
COMPUTATIONAL ANALYSIS;
CRITICAL FAILURES;
CRITICAL STIFFNESS;
CRITICAL SURFACES;
DESIGN/METHODOLOGY/APPROACH;
FEM MODELS;
FLUTTER ANALYSIS;
GROUND VIBRATION TESTS;
HIGH RELIABILITY;
MODELLING;
MSC.NASTRAN;
NASTRAN SOFTWARE;
NATIONAL PROJECTS;
NONLINEAR PROPERTIES;
NORMAL VIBRATIONS;
REDUCED STIFFNESS;
REMOTE HANDLING DEVICES;
RESEARCH LIMITATIONS;
RESEARCH VEHICLES;
RESONANT MODE;
ROTATIONAL MODES;
SAFETY LEVEL;
STABILISATION;
TEST RESULTS;
ACTUATORS;
AEROELASTICITY;
AIRCRAFT;
AIRCRAFT CONTROL;
CONTROL SYSTEMS;
EMPENNAGES;
FLIGHT CONTROL SYSTEMS;
FLUTTER (AERODYNAMICS);
RESEARCH;
SOFTWARE TESTING;
STIFFNESS;
UNMANNED AERIAL VEHICLES (UAV);
UNMANNED VEHICLES;
VERIFICATION;
CONTROL SURFACES;
|
|
EID: 79957852707
PISSN: 17579864
EISSN: 17579872
Source Type: Journal
DOI: 10.1108/17579861111135914 Document Type: Article |
|
Times cited : (6)
|
|
References (5)
|
