Title: Designing an adaptive robust observer for underactuation fault diagnosis of SSS-1 satellite. By Mohammad Zarourati Supervisor: Dr. Mehran Mirshams Advisor: Dr. Morteza Tayefi Chairmen: Dr. Abdolmajied Khoshnood (K. N. Toosi University of Technology) December 11, 2022
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 [...]
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 [...]
Congratulations, Niki Sajad, PhD student and the head of SRL ‘s simulation office has been awarded by IAC2022 , Read more
APSCO SSS project FRR meeting started! More info
Space Professionals Webinar Held on Sunday, May 8th 4:00 - 6:00 PM Kuwait Time
Ph. D. Thesis Author Introduction: First name: Mohammad Last name: Zarourati Entrance year: 2019 Defense date: 2024/Jan/17 Email address: zarourati@email.kntu.ac.ir Title: Attitude Control of a Remote Sensing Satellite in Underactuated Conditions Abstract: Underactuation poses a significant challenge to space mission control and performance. This dissertation investigates the non-linear attitude tracking control problem for a remote sensing satellite underactuated by a reaction wheel (RW) actuator fault. First, the fault detection and diagnosis strategy is based on the sliding mode and adaptive sliding mode observers in a finite-time decision window. The failed actuator is excluded from the control [...]
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 [...]
SRL team took part in the exhibition Space Technology capacities held by the Iranian space agency and ICT ministry. SRL introduced the CubeSat hands-on training packages and their capabilities to the ICT minister, Iranian Space Agency head, and visitors in this exhibition.
Space Maneuvers Simulation Room and its infrastructure, step by step, are becoming ready for Operational Tests.
Space Research Laboratory, Aerospace Engineering Faculty, K. N. Toosi University of Technology, Daneshgah Blvd., Ehsan Exit, East Zeynoddin Highway, Tehran, Iran
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