Wheel fixed (13 Ergebnisse)

Zustand: Very Good. Pages intact with possible writing/highlighting. Binding strong with minor wear. Dust jackets/supplements may not be included. Stock photo provided. Product includes identifying sticker. Better World Books: Buy Books. Do Good.

Unknown binding. Zustand: Good. Paperback. Pages are clean and unmarked. Covers show light edge wear.; 100% Satisfaction Guaranteed! Ships same or next business day.

PAP. Zustand: New. New Book. Shipped from UK. Established seller since 2000.

PAP. Zustand: New. New Book. Shipped from UK. Established seller since 2000.

Hardcover. Zustand: Very Good. Zustand des Schutzumschlags: Good. First Edition. First ed, stated. Jacket in mylar, minor shelf/age wear, clean. General shelf/age wear. Pages/boards clean.

HRD. Zustand: New. New Book. Shipped from UK. Established seller since 2000.

HRD. Zustand: New. New Book. Shipped from UK. Established seller since 2000.

Hardcover. Zustand: Very Good. Little, Brown and Company Boston, MA January 1951 Binding: Hardcover.

Hardcover. Zustand: Very good. Hardcover. First Edition. Very good hardback in a tanned and lightly edgeworn jacket.

Hardcover/Pappeinband. 180 Zufriedenstellend / Bibliotheksexemplar / Sprache: Deutsch Gewicht in Gramm: 350.

Taschenbuch. Zustand: Neu. Neuware - Attitude determination of satellites is normally the job of inertial instruments, such as gyroscopes, or through sensing instruments, such as star trackers orGlobal Positioning Satellites (GPS). Satellite health monitoring systems watch and determine if the satellite deviates from its normal operating attitudeorientation. Knowing the orientation of a satellite is essential in being able to control it in order to complete the satellite's designated mission. While there area multitude of ways to determine a satellite's orientation, very little research has been done on determining if the attitude of a satellite can be determineddirectly from telemetry data of the attitude control systems and an accurate spacecraft model. The fidelity of a satellite attitude determination model requiredto get reasonable predictions from using only telemetry data of the attitude controllers, such as thruster on/off indicators and reaction wheel rotor speeds, isinvestigated. Experimental tests using telemetry data received from the Air Force Institute of Technology's (AFIT) Simulated Satellite, SimSat, is used inverifying a Matlab model which outputs SimSat's orientation from SimSat's reaction wheel and thruster telemetry data. Software modeling results showed thatit is possible to determine a satellite's attitude from only the attitude controllers' telemetry data when the satellite's dynamic model is known.This work has been selected by scholars as being culturally important, and is part of the knowledge base of civilization as we know it. This work was reproduced from the original artifact, and remains as true to the original work as possible. Therefore, you will see the original copyright references, library stamps (as most of these works have been housed in our most important libraries around the world), and other notations in the work.This work is in the public domain in the United States of America, and possibly other nations. Within the United States, you may freely copy and distribute this work, as no entity (individual or corporate) has a copyright on the body of the work.As a reproduction of a historical artifact, this work may contain missing or blurred pages, poor pictures, errant marks, etc. Scholars believe, and we concur, that this work is important enough to be preserved, reproduced, and made generally available to the public. We appreciate your support of the preservation process, and thank you for being an important part of keeping this knowledge alive and relevant.…

Buch. Zustand: Neu. Neuware.

180 S., 12 S. Verlagsanzeigen. Rotes Leinen mit Schutzumschlag. Gebrsp. Umschlag berieben, oben etwas eingerissen. Buchblock papierbedingt gebräunt. Vorderer fliegender Vorsatz mit kleinem Ausschnitt. Deutsche Erstausgabe. Schutzumschlag von Eyke Volkmer.