Pages that link to "Item:Q786105"
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The following pages link to Analytical algorithm for constructing the orbital orientation of a spacecraft with an incomplete measurement of the state vector components (Q786105):
Displaying 5 items.
- Synthesis of stabilizing spacecraft control based on generalized Ackermann's formula (Q356984) (← links)
- Application of Cayley-Klein parameters in the problem of strapdown navigation system stochastic state vector synthesis for a self-contained space vehicle (Q1003006) (← links)
- Terminal synthesis of orbital orientation for a spacecraft (Q1745868) (← links)
- Reducing the problem of the modal control by output for stationary fourth-order systems with two inputs and two outputs to the control by state for a system with a single input (Q6137173) (← links)
- Analytical synthesis of an aircraft's lateral motion control by output at the lack of measurements of slip and roll angles (Q6178139) (← links)
