The Use of a System of Variable Structure to Control the Flight Range of a Spacecraft Reentering the Earths Atmosphere

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The Use of a System of Variable Structure to Control the Flight Range of a Spacecraft Reentering the Earths Atmosphere

I. S. Ukolov / Y. A. Tyurin / E. I. Mitroshin / B. N. Petrov

A method of constructing a control system is proposed that uses nonlinear systems. It is found that using systems of variable structure to control a re-entering spacecraft provides low sensitivity to changes in the spacecraft parameters. (Author)

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Titel :

The Use of a System of Variable Structure to Control the Flight Range of a Spacecraft Reentering the Earths Atmosphere

Beteiligte:

I. S. Ukolov (Autor:in) / Y. A. Tyurin (Autor:in) / E. I. Mitroshin (Autor:in) / B. N. Petrov (Autor:in)

Erscheinungsdatum :

1972

Format / Umfang :

20 pages

Medientyp :

Report

Format :

Keine Angabe

Sprache :

Englisch

Schlagwörter :

Manned Spacecraft , Guidance Systems , Atmospheric entry , Reentry physics , Spacecraft control , Spacecraft design , Equipment specifications , Systems analysis , Systems engineering , Translations

The Use of a System of Variable Structure to Control the Flight Range of a Spacecraft Reentering the Earths Atmosphere

The Use of a System of Variable Structure to Control the Flight Range of a Spacecraft Reentering the Earths Atmosphere

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