wheel fixed (11 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.

Paperback. Zustand: Good. No Jacket. Pages can have notes/highlighting. Spine may show signs of wear. ~ ThriftBooks: Read More, Spend Less.

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

Zustand: Good. First edition copy. . Good dust jacket. Dust jacket price clipped. In protective mylar cover. (California, Murder, Detectives, Mystery).

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.

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.

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.