System model for Earth observation missions

Paper number

IAC-13,D1,3,6,x18387

Author

Dr. Marat Nurguzhin, JSC «National Company «Kazakhstan Gharysh Sapary», Kazakhstan

Coauthor

Dr. S Murushkin, JSC «National Company «Kazakhstan Gharysh Sapary», Kazakhstan

Coauthor

Dr. Vladimir Ten, Kazakhstan Gharysh Sapary, Kazakhstan

Coauthor

Mr. Arman Bekembayev, Kazakhstan Gharysh Sapary, Kazakhstan

Year

2013

Abstract

Many companies in the space industry at some point find the need of a detailed system model for mission design and sizing of satellite subsystems including solar panels area, battery capacity, downlink rate and many others. Our model is being developed in-house which is a typical situation as no existing products on the market are flexible enough for specific cases and types of analysis.

The paper reviews the system model that was initially intended just for quick preliminary analysis and sizing of different types of Earth Observation missions and that is now evolving to integrated, flexible, user-friendly tool for detailed mission design and sizing.

This paper will also describe the use of the system model for Earth Observation missions: typical tasks to solve and the way those tasks are dealt with in the system model.

Abstract document

IAC-13,D1,3,6,x18387.brief.pdf

Manuscript document

IAC-13,D1,3,6,x18387.pdf (🔒 authorized access only).

To get the manuscript, please contact IAF Secretariat.