000	02233nam  2200385zi 4500
001	9.892809
003	CaOODSP
005	20221107173255
006	m     o  d f
007	cr bn|||||||||
008	201023s1970    onca    ob   f000 0 eng d
040	|aCaOODSP|beng|erda|cCaOODSP
086	1 |aCo24-3/7-1212-1970E-PDF
100	1 |aVigneron, F. R., |eauthor.
245	10|aStability of a dual spin satellite with two dampers in circular orbit / |cby F.R. Vigneron.
264	1|aOttawa : |bCommunications Research Centre, |c1970.
300	|a1 online resource (iii, 24 pages) : |billustrations.
336	|atext|btxt|2rdacontent
337	|acomputer|bc|2rdamedia
338	|aonline resource|bcr|2rdacarrier
490	1 |aCRC report ; |vno. 1212
500	|a"National Space Telecommunications Laboratory."
500	|a"Published December 1970."
500	|aDigitized edition from print [produced by Innovation, Science and Economic Development Canada].
504	|aIncludes bibliographical references (pages 21-22).
520	3 |a"The motion of a dual spin satellite in circular orbit is studied to determine the effect of gravitational torques and damping when the spin vector is approximately normal to the orbit plane. Stability results are assessed by the Floquet method for selected cases to show that gravitational torques are important when spin rates are low. Solutions are obtained analytically for high spin cases using the method of averaging to demonstrate the effect of gravitational torque and damping on both rotor and despun platform. For the high spin cases, stability criteria are identical with criteria previously derived for a freely spinning untorqued dual spin satellite"--Abstract, page 1.
530	|aIssued also in print format.
650	0|aArtificial satellites|xStability.
650	0|aDamping (Mechanics)
650	6|aSatellites artificiels|xStabilité.
650	6|aAmortissement (Mécanique)
710	2 |aCommunications Research Centre (Canada), |eissuing body.
830	#0|aCRC report ;|vno. 1212.|w(CaOODSP)9.882492
856	40|qPDF|s1.27 MB|uhttps://publications.gc.ca/collections/collection_2020/isde-ised/Co24/Co24-3-7-1212-1970-eng.pdf