Research graph
References from Thermoelastic vibration and maneuver control of smart satellites. Local targets link to admitted publications; unresolved targets remain external evidence.
Vibration suppression of smart nonlinear flexible appendages of a rotating satellite by using hybrid adaptive sliding mode/Lyapunov control
10.1177/1077546312439913 · 2013 · External reference
Vibration suppression and adaptive-robust control of a smart flexible satellite with three axes maneuvering
2011 · External reference
Dynamics and control of a smart flexible satellite moving in an orbit
10.1007/s11044-014-9447-2 · 2015 · External reference
Active control of an fgm beam under follower force with piezoelectric sensors/actuators
10.1142/s0219455413500636 · 2014 · External reference
Thermal analysis of a reflective baffle designed for space applications
2011 · External reference
Unresolved reference
2012 · External reference
Wavelet technique applied to dynamic response of thin-walled composite booms exposed to solar radiation
2003 · External reference
Sunrise/Sunset thermal shock disturbance analysis and simulation for the TOPEX satellite
1990 · External reference
Attitude maneuver control of a two-wheeled spacecraft with bounded wheel speeds
10.1016/j.actaastro.2013.03.006 · 2013 · External reference
Sliding mode attitude control with L 2-gain performance and vibration reduction of flexible spacecraft with actuator dynamics
2010 · External reference
Dynamics and control of spacecraft hovering using the geomagnetic Lorentz force
10.1016/j.asr.2013.11.040 · 2014 · External reference
Spacecraft attitude maneuver using two single-gimbal control moment gyros
10.1016/j.actaastro.2012.07.035 · 2013 · External reference
Analytical and numerical approaches of a solar array thermal analysis in a low-earth orbit satellite
10.1016/j.asr.2010.08.023 · 2010 · External reference
Thermal analysis of composite solar array subjected to space heat flux
10.1016/j.ast.2012.06.010 · 2013 · External reference
Unresolved reference
1997 · External reference
Dynamic response control of rotating composite booms under solar radiation
2008 · External reference
Vibration reduction of flexible solar array during orbital maneuver
10.1108/aeat-05-2012-0072 · 2014 · External reference
Active vibration control of spatial flexible multibody systems
10.1007/s11044-013-9341-3 · 2013 · External reference
Unresolved reference
1993 · External reference
Passive vibration control of flexible spacecraft using shunted piezoelectric transducers
10.1016/j.ast.2013.05.001 · 2013 · External reference
Thermally induced vibrations of flexible beams using Absolute Nodal Coordinate Formulation
10.1016/j.ast.2013.04.009 · 2013 · External reference
Thermally induced bending vibration of composite spacecraft booms subjected to solar heating
10.1080/01495730306307 · 2003 · External reference
Rapid rotational maneuvering of rigid satellites with hybrid actuators configuration
10.2514/1.56405 · 2013 · External reference
Rapid rotational maneuvering of rigid satellites with reaction wheels
10.2514/1.58155 · 2013 · External reference
Nonlinear optimal control of spacecraft approaching a tumbling target
10.1016/j.ast.2010.05.009 · 2011 · External reference
Thermally-induced bending-torsion coupling vibration of large scale space structures
10.1007/s00466-006-0134-x · 2007 · External reference
Stability of thermally induced vibration of a beam subjected to solar heating
10.2514/1.j052574 · 2014 · External reference
