Thesis (Ph. D.)


Ph. D. Thesis Author Introduction: First name: Ehsan Last name: Zabihian Entrance year: 2012 Defense date: 2018/Apr/28 Email address:, Title: New Algorithm for GEO Communication Satellite Conceptual Design Abstract: This thesis describes a new methodlogy design approach for GEO geostationary communication satellite. This method has been developed to reduce the prohibitive cost and time of their conceptual design phase. The proposed method effectively conducts the design of GEO communication satellite lying in the range of 1–7 thousand kilograms. The main feature of the new methodlogy is to determine the design information of the conceptual [...]

Thesis (Ph. D.) 2022-05-09T06:18:01+00:00



Title: Attitude path design and adaptive robust tracking control of a remote sensing satellite in various imaging modes Journal: Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering Authors: Mohammad Zarourati, Mehran Mirshams, Morteza Tayefi Available online: January 2, 2023. DOI Title: FADSat: A system engineering tool for the conceptual design of geostationary Earth orbit satellites platform Journal: Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering Authors: Mehran Mirshams, Ehsan Zabihian Available online: May 3, 2018. DOI Title: Mass properties identification and automatic mass balancing system [...]

Papers 2023-01-17T06:01:44+00:00

Thesis (M. Sc.)


M. Sc. Thesis Author Introduction:First name: ShahramLast name: KeshavarziEntrance year: 2020Defense date: 2023/Sep/12Email address: Title: Autonomous optical navigation of interplanetary cubesats Abstract: Mission planning for space exploration typically relies on determining the Earth orbit to determine the appropriate position and guide the spacecraft towards the mission objective. This process involves ground tracking stations and flight dynamics teams for communication and control of spacecraft in deep space, contributing to the overall cost of space missions. However, recent expansion of CubeSat satellites challenges this paradigm, where interplanetary spacecraft navigations are employed. In fact, miniature spacecraft increase the total number [...]

Thesis (M. Sc.) 2023-10-04T05:08:06+00:00

Contact Info

Space Research Laboratory, Aerospace Engineering Faculty, K. N. Toosi University of Technology, Daneshgah Blvd., Ehsan Exit, East Zeynoddin Highway, Tehran, Iran

Phone: +98 21 77334133

Fax: +98 21 73064234

Web: Spacerl

Recent Posts