Publication

/Publication

Thesis (Ph. D.)

2024-02-07T06:50:32+00:00

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 [...]

Thesis (Ph. D.) 2024-02-07T06:50:32+00:00

Papers

2023-01-17T06:01:44+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.)

2024-09-25T11:33:28+00:00

M. Sc. Thesis Author Introduction: First name: Mohammad Last name: Akhtari Entrance year: 2021 Defense date: 2024/August/06 Email address: m.akhtari@email.kntu.ac.ir Title: Implementation of Asteroid Rendezvous Maneuvers in a Hardware in-the-Loop Setup Abstract: This project aims to design, develop, and test a simulation platform for space maneuvers and proximity operations with asteroids. Initially, a three-degree-of freedom air-bearing testbed was constructed, featuring two translational degrees and one rotational degree to simulate the operational environment of a spacecraft. Subsequently, a "dark room" was equipped and set up to mimic space conditions for testing and maneuver operations, ensuring a highly [...]

Thesis (M. Sc.) 2024-09-25T11:33:28+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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