Pages that link to "Item:Q4961690"
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The following pages link to Optimal stabilization of spacecraft in an inertial coordinate system based on a strapdown inertial navigation system (Q4961690):
Displaying 6 items.
- Application of Cayley-Klein parameters in the problem of strapdown navigation system stochastic state vector synthesis for a self-contained space vehicle (Q1003006) (← links)
- Influence of seeker disturbance rejection and radome error on the Lyapunov stability of guidance systems (Q1720498) (← links)
- Inverse optimal stabilization of a rigid spacecraft (Q4506798) (← links)
- An integrated solution to ACMM problem of spacecraft with inertia uncertainty (Q4626646) (← links)
- (Q4668833) (← links)
- On the spacecraft attitude stabilization in the orbital frame (Q5403494) (← links)