Akademik Veri Yönetim Sistemi
AIAA Modeling and Simulation Technologies Conference 2010, Toronto, Kanada, 2 - 05 Ağustos 2010
Magnetic controllers for maintaining and varying spacecraft's directivity using only magnetorquers are presented using dynamic attitude simulator environment (DASE), which includes a flight computer and the complete satellite communications architecture. Magnetorquers are environmental actuators that on the contrary to reaction wheels do not have any moving parts. For that reason using only magnetorquers for the tasks where precise attitude control is not required prolongs mission lifetime. Despite the inability to produce torque along the Earth's magnetic field vector magnetorquers can still provide the sufficient pointing accuracy for the on-board antennae with help of B-max and VBC controllers. The controllers are designed for RASAT, an Earth observation satellite, to be launched to a sun-synchronous low Earth orbit (LEO) orbit. The satellite ground communication is achieved via rigidly mounted X-band and S-band antennae with restricted radiation patterns. The controllers' purpose is to maximize the high speed communication duration by directing the satellite's side where the antennae are located towards the ground station during each pass. The results show that magnetic actuation provides sufficient pointing accuracy that surpasses the Nadir-pointing flight mode in terms of communication duration. © 2010 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.