Method of Slewing the Spacecraft to Minimize Settling Time

First Page		Document Content
Date: 2013-06-21 18:13:17 Systems theory Science Input shaping Torque Vibration Feedback Bang–bang control Control theory Cybernetics Physics		Method of Slewing the Spacecraft to Minimize Settling Time Add to Reading List Source URL: www.nps.edu Download Document from Source Website File Size: 323,68 KB Share Document on Facebook

	Search, Align, and Repair: Data-Driven Feedback DocID: 1xVRZ - View Document
	ZKProof Standards Security Track Proceedings 1 August 2018 + subsequent revisions This document is an ongoing work in progress. Feedback and contributions are encouraged. Track chairs: DocID: 1xVIQ - View Document
	ZKProof Standards Applications Track Proceedings 1 August 2018 + subsequent revisions This document is an ongoing work in progress. Feedback and contributions are encouraged. Track Chairs: DocID: 1xUWk - View Document
	ZKProof Standards Implementation Track Proceedings 1 August 2018 + subsequent revisions This document is an ongoing work in progress. Feedback and contributions are encouraged. Track chairs: DocID: 1xULZ - View Document
	DECENTRALIZED HIGH QUALITY MARKET FEEDBACK PLATFORM ReviewNetwork Our Mission DocID: 1xUqF - View Document