Published November 1969
| Published
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Atmospheric re-entry into the Martian atmosphere with variable lift control
- Creators
- Ohtakay, Hiroshi
Abstract
A gliding type re-entry of a space capsule into the Martian atmosphere for softlanding with the minimum heat generation is investigated. A nonlinear filter which can be installed on-board is developed to estimate the unknown atmospheric parameter values of Mars in real-time. A stochastic control problem with state variables estimation is investigated for the re-entry capsule which is subject to random movements of the Martian atmosphere due to wind and wind gusts.
Additional Information
© 1969 IEEE. A part of this work was done when the author was a summer employee with Jet Propulsion Laboratory, Callfornia Institute of Technology, under Contract No. NAS 7-100, sponsored by the National Aeronautics and Space Administration.Attached Files
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04044557.pdf
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Additional details
- Eprint ID
- 80388
- Resolver ID
- CaltechAUTHORS:20170814-160638759
- NAS 7-100
- NASA/JPL/Caltech
- Created
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2017-08-15Created from EPrint's datestamp field
- Updated
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2021-11-15Created from EPrint's last_modified field