Pages that link to "Item:Q393688"
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The following pages link to Integrated navigation system for a space vehicle on a geostationary or highly elliptic orbit operating in the presence of active jam (Q393688):
Displaying 6 items.
- An optimal discrete nonlinear logical-dynamical filter-predictor (Q393662) (← links)
- Autonomous navigation during the final ascent of a spacecraft into the geostationary orbit. Autonomous integrated navigation system concept (Q1742394) (← links)
- Analysis of conditions for ensuring operation of an intertial satellite navigation system of an unmannded aerial vehicle during interference (Q1956896) (← links)
- Optimal injection of a satellite into geostationary orbit using a limited number of thruster firings (Q2017634) (← links)
- A solution of the navigation problem for autonomous insertion of payload into a geostationary orbit using a low-thrust engine (Q2515396) (← links)
- On the properties of the limit control sets for a class of unstable linear systems with discrete time and \(l_1\)-restrictions (Q2695124) (← links)
