FIELD: aircraft engineering.
SUBSTANCE: invention relates to the control over the spacecraft, mainly, at the orbiting path atmospheric section. Claimed process comprises the online by onboard means of the altitude of the path pericentre immediately after the spacecraft re-entry. Then, the reactive correction of said path nearby the entry corridor lower boundary is performed. At skipping, the optimum control programs are operated for control over aerodynamic forces before spacecraft exit from atmosphere. Note here that the spacecraft flight nearby said entry corridor lower boundary can be performed in more rarefied atmosphere layers to ensure the higher speed at the transition orbit apocentre. At said apocentre the spacecraft receives the extra acceleration pulse to generate the preset orbit of the planet artificial satellite.
EFFECT: higher efficiency of control, decreased consumption of fuel.
2 dwg
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SU1838177A3 |
