Trajectory Control for a Spacecraft with an Inflatable Braking Device in the Martian Atmosphere

Details Trajectory Control for a Spacecraft with an Inflatable Braking Device in the Martian Atmosphere Trajectory Control for a Spacecraft with an Inflatable Braking Device in the Martian Atmosphere

May 2003

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=2003cosre..41..280a&link_type=abstract

Cosmic Research, v. 41, Issue 3, p. 280-284 (2003).

Computer Science

Scientific paper

The possibility of using an inflatable braking device for controlled
descent in the Martian atmosphere of large-capacity cargoes is analyzed.
The most complicated version of the trajectory control problem is
considered, namely, the injection of a spacecraft at hyperbolic velocity
into a parking orbit after braking in the atmosphere.

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