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Niki Sajjad participated in the SGC and IAC 2022

2022-11-01T11:16:13+00:00

Niki Sajjad participated in the 20th Space Generation Congress (SGC) and the 73rd International Astronautical Congress (IAC) in Paris from 13 to 22 September. Niki was one of the 30 students and young professionals from across the globe to be selected as the 2022 IAF Emerging Space Leaders grantee and got an invaluable opportunity to network with experts and present her work in front of the key players in the space sector. She also won the SGC logo competition and could participate in this congress for the second consecutive year. During the SGC, Niki participated in the Planet’s working group [...]

Niki Sajjad participated in the SGC and IAC 2022 2022-11-01T11:16:13+00:00

A Thesis Defense Session for MSc/Mahdi Rivandi

2022-09-26T07:49:36+00:00

Title: Upgrade balance system for CubeSat attitude simulator based on the air bearing platform By Mahdi Rivandi Supervisor: Dr. Mehran Mirshams Advisor: Mr. Mohammad Zarorati Chairmen: Dr. Mahdi Jafari Nadoushan (K. N. Toosi University of Technology), Dr. Mohammad Ali Noorian (K. N. Toosi University of Technology) September 22, 2022 In order to test the attitude control of a satellite, it is necessary to have attitude control simulator, and this simulator must also be placed in the condition of balance, including weight. This thesis was carried out in the form of simulation and implementation, to simulate the deviations [...]

A Thesis Defense Session for MSc/Mahdi Rivandi 2022-09-26T07:49:36+00:00

Thesis (Ph. D.)

2022-05-09T06:18:01+00:00

Ph. D. Thesis Author Introduction: First name: Ehsan Last name: Zabihian Entrance year: 2012 Defense date: 2018/Apr/28 Email address: e.zabihian@mail.kntu.ac.ir, e.zabihian@hotmail.com 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

A Thesis Defense Session for MSc/Morteza Abbasi

2022-03-07T07:21:27+00:00

Title: Simulation and implementation of interplanetary CubeSat closed-loop attitude control based on the air-bearing platform By Morteza Abbasi Supervisor: Dr. Mehran Mirshams Advisors: Ms. Niki Sajjad Chairmen: Dr. Alireza Basohbat Novinzad (K.N. Toosi University of Technology), Dr. Abdolmajid Khoshnood (K.N. Toosi University of Technology) March 2, 2022 Abstract: With the increasing expansion of interplanetary missions and space exploration, flight control, guidance, and navigation programs for space systems have become very important. In this research, we first design and develop a suitable test platform to simulate the operating environment of the spacecraft in performing orbital missions, such as orbital maneuvers, orbital [...]

A Thesis Defense Session for MSc/Morteza Abbasi 2022-03-07T07:21:27+00:00

A Thesis Defense Session for MSc/ Mojtaba Namvar

2022-04-11T06:56:02+00:00

Title: Electro-optical orbit determination with using the COTS equipment By Mojtaba NamvarSupervisor: Dr. Mehran MirshamsAdvisors: Alireza VafaChairmen: Dr. Hamed Alisadeghi (K. N. Toosi University of Technology), Dr. Alireza Basohbat Novinzad (K. N. Toosi University of Technology)January 12, 2022 Determining the orbits of satellites is essential for planning and carrying out space projects. As in the past, the issue of determining the orbits of planets and objects in space has been considered by scientists, with the pervasiveness of space missions and the increase in the number of satellites, the need for continuous monitoring of space is increasingly considered by space organizations [...]

A Thesis Defense Session for MSc/ Mojtaba Namvar 2022-04-11T06:56:02+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

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