Pages that link to "Item:Q2307026"
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The following pages link to Dynamical modeling and attitude analysis for the spacecraft with lateral solar arrays (Q2307026):
Displaying 12 items.
- Dynamics of a rotating flexible and symmetric spacecraft using impedance matrix in terms of the flexible appendages cantilever modes (Q934768) (← links)
- Dynamics of satellite with deployable rigid solar arrays (Q1035407) (← links)
- Thermal alternation induced vibration analysis of spacecraft with lateral solar arrays in orbit (Q2049751) (← links)
- Study on analytical global modes for a multi-panel structure connected with flexible hinges (Q2056650) (← links)
- Determining the parameters of a mathematical model of spacecraft solar batteries from telemetry data (Q2058712) (← links)
- Dynamic modeling and analytical global mode shapes of a folded beam-ring structure for a truss antenna reflector with two arms (Q2110048) (← links)
- Rigid-flexible coupling effect on attitude dynamics of electric solar wind sail (Q2219601) (← links)
- Optimization design method for kirigami-inspired space deployable structures with cylindrical surfaces (Q2245847) (← links)
- A brief analysis of artificial satellites solar panels deployment considering a nonlinear dynamic model (Q2679181) (← links)
- (Q3307584) (← links)
- (Q3446447) (← links)
- (Q4487151) (← links)