Pages that link to "Item:Q353711"
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The following pages link to Control of angular motion of a landing module of ``Soyuz'' type upon satellite returning from the orbit (Q353711):
Displaying 4 items.
- History of spacecraft control systems (Q358288) (← links)
- Analysis of the reasons for an aerodynamic hysteresis in flight tests of the Soyuz reentry capsule at the hypersonic segment of its descent (Q369203) (← links)
- Synthesis of decoupling laws for controlling the angular motion of landing module with solid-fuel landing engine minimizing the transient time (Q393690) (← links)
- Correction of a strapdown inertial navigation system during descent in the atmosphere (Q2699167) (← links)