|Statement||edited by S. Fred Singer.|
|Series||Applied mathematics and mechanics,, v. 7|
|LC Classifications||TL3260 .S56 1964|
|The Physical Object|
|Pagination||xiii, 261 p.|
|Number of Pages||261|
|LC Control Number||64015274|
Applied Mathematics and Mechanics, Volume 7: Torques and Attitude Sensing in Earth Satellites focuses on the possible torques that can affect the angular momentum of an Earth satellite. This book provides an understanding of the environment in which a satellite operates. Additional Physical Format: Online version: Singer, S. Fred (Siegfried Fred), Torques and attitude sensing in earth satellites. New York, Academic Press, Torques and attitude sensing in earth satellites, by S. Fred Singer (Author) See all 2 formats and editions Hide other formats and editions. Price New from Used from Kindle "Please retry" $ — Author: S. Fred Singer. Torques and attitude sensing in earth satellites. New York, Academic Press, (DLC) (OCoLC) Material Type: Document, Internet resource: Document Type: Internet Resource, Computer File: All Authors / Contributors: S Fred Singer.
Torques and Attitude Sensing in Earth Satellites, Fred Singer, emne: naturvidenskab, Book Title: Torques and Attitude Sensing in Earth Satellites Author: Fred Singer ASIN: BYGKG6 All the books listed here are written in english, so the descriptions are also in English. Postage is 39kr postage with GLs Pakkeshop uden omdeling, Condition: Hardback edition with DJ, plastic cover, clean pages. Attitude control is the process of controlling the orientation of an aerospace vehicle with respect to an inertial frame of reference or another entity such as the celestial sphere, certain fields, and nearby objects, etc.. Controlling vehicle attitude requires sensors to measure vehicle orientation, actuators to apply the torques needed to orient the vehicle to a desired attitude, and. Explain the elements of space vehicle attitude determination and control subsystems and describe various technologies currently in use (enrichment topic) Outline Control Systems Attitude Control Having the Right Attitude Attitude Dynamics Disturbance Torques Spacecraft Attitude Sensors Spacecraft Attitude Actuators The. joined by other Earth-observing satellites. This weather must be either stored or removed by the attitude system. Small external torques that vary over the course of an properties, required accuracy, orbit or other sensing devices. geometry, mission lifetime, space Control actuators: reaction wheels.
Attitude jitter is a problem commonly experienced by remote-sensing satellites, and deteriorates the accuracy of geo-positioning and mapping. Therefore, it is important to design a method which Author: Akira Iwasaki. PDF | A method to analyze the stability of satellites flying in low Earth orbits is presented. Starting from the classical rotational equations of | Find, read and cite all the research you. In this paper a survey is made of some aspects of satellite attitude stabilization and control. After a brief discussion of the equations of motion governing the satellite's behaviour, the various disturbing torques acting on a satellite in a space environment are considered. Quantitative values for a hypothetical satellite are discussed. Next, attention is given to several methods of attitude Cited by: Applied Mathematics and Mechanics, Volume 7: Torques and Attitude Sensing in Earth Satellites focuses on the possible torques that can affect the angular momentum of an Earth satellite. This book provides an understanding of the environment in which a satellite operates. Organized into 16 chapters, this volume starts with an overview of the application of force-free motion to space programs.