A constraint-based technique to choose design parameters of spacecraft versions meant for earth remote sensing

Spacecraft and Rockets


Аuthors

Matveev Y. A.*, Lamzin V. V.**

Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia

*e-mail: matveev_ya@mail.ru
**e-mail: 8916846583@mail.ru

Abstract

Methodological aspects are considered for design investigations to update effectively space systems intended for earth remote sensing (ERS). A statement of the constrained update problem is discussed. An example is given to demonstrate effective updating process for the some ERS space system.

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