Spacecraft Dynamics and Control

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• GÖKHAN İNALHAN

this paper may be made for personal or internal use, on condition that the copier pay the $10.00 per-copy fee to the Copyright Clearance Center, Inc., 222 Rosewood Drive, Danvers, MA 01923; include the code 0731-5090 /02 $10.00 in correspondenc e with the CCC

Abstract Formation flying of multiple spacecraft is an enabling technology for many future space science missions. However, the co‐ordination and control of these instruments poses many difficult design challenges. This paper presents fuel/time‐optimal control algorithms for a co‐ordination and control architecture th…

• GÖKHAN İNALHAN

Formation #ying of multiple spacecraft is an enabling technology for many future space science missions. However, the coordination and control of such instruments present many design challenges. This paper addresses the formation #ying spacecraft control problem at several levels. We presentlow-level, multi-vehicle, s…

Formation flying of multiple spacecraft is an enabling technology for future space science missions such as separated spacecraft interferometers. Controllers designed for these multi-vehicle fleets must address many high- and low-level tasks, and will become very complicated for large fleets. As such, this work descri…

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There has been increasing interest in satellite design and manufacture. Satellites require complex components that must withstand severe mechanical and thermal conditions. Thermal design of a satellite relies on several dynamic factors. Satellites experience both extreme temperatures and rapid temperature changes. Thi…

• METİN AKTAŞ

This article describes the control of a rotary inverted pendulum utilizing on–off-type cold gas thrusters as the actuators, which have high similarities with thruster actuated spacecrafts with slosh dynamics. The study is completed in three phases. Firstly, a Pulse Width Modulator (PWM) design method is utilized to ob…

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• ÖZGÜN YÜCEL

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• ÖZNUR KAYHAN

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• ASLI ELMASLI AKÇAR
• SELİM OSMAN SELAM