Pages that link to "Item:Q2214171"
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The following pages link to Mathematical simulation of satellite motion with an aerodynamic attitude control system influenced by active damping torques (Q2214171):
Displaying 3 items.
- Modeling and numerical simulation of linear and nonlinear spacecraft attitude dynamics and gravity gradient moments: a comparative study (Q430373) (← links)
- A way for accelerated calculation of spacecraft motion in an atmosphere with a tethered aerodynamic stabilizer (Q2961180) (← links)
- (Q3427999) (← links)