Space Science and Technology

Space subsystems design: (navigation, control, structure and…)

Attitude Control of Nanosatellite Using Optimal Quadratic Linear and Nonlinear Methods

Arash Abarghooei; Hassan Salarieh; Pedram Hosseiniakram

Volume 16, English Special Issue , November 2023, , Pages 51-64

Abstract

Linear algorithms are the most widely used method for satellite attitude control using reaction wheels because of their simplicity and low computational cost. The first part of the paper introduces different attitude determination and control algorithms, and reviews resources that utilized optimal linear ... Read More

Multidisciplinary Conceptual Design Optimization of Monopropellant Propulsion System of Nanosatellite

M. Nosratollahi; A. h. Adami-Dehkordi

Volume 3, Issue 2 , January 2011, , Pages 11-22

Abstract

This paper presents the multidisciplinary design optimization of monopropellant propulsion system of the nanosatellite for planner maneuver. Mass, configuration and internal ballistic equations are derived for any part of propulsion system (thruster, tank, pressurized gas, ...). Minimizing total mass ... Read More

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Keywords = nanosatellite

Attitude Control of Nanosatellite Using Optimal Quadratic Linear and Nonlinear Methods

Abstract

Multidisciplinary Conceptual Design Optimization of Monopropellant Propulsion System of Nanosatellite

Abstract