Patent · US Active

Propulsive guidance for atmospheric skip entry trajectories

US8489258B2 · kind B2 · utility

0Cited by
13References
17Claims
0Family size

Assignee

Inventors

Key dates

Filing dateMar 26, 2010
Grant dateJul 16, 2013
Priority date
Expiry dateOct 5, 2031

Classification

  • Technology area (CPC G)Physics
  • CPC primaryG01C21/24
  • WIPO fieldMeasurement
  • WIPO sectorInstruments

Abstract

The invention set forth herein describes propulsive guidance methods and apparatus for controlling and shaping an atmospheric skip reentry trajectory for a space vehicle. Embodiments of the invention may utilize a powered explicit guidance algorithm to provide a closed-loop control method for controlling a space vehicle during a skip reentry maneuver.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.