000	00000nam 2200000zi 4500
001	9.942491
003	CaOODSP
005	20241104141611
006	m     o  d f
007	cr |n|||||||||
008	240827e198410##oncda   ob   f000 0 eng d
040	|aCaOODSP|beng|erda|cCaOODSP
041	1 |aeng|bfre
043	|an-cn---
086	1 |aDR52-18/43-1984E-PDF
100	1 |aVinnins, Michael, |d1952- |eauthor.
245	10|aTest evaluation of the Honeywell GG1111 single-degree-of-freedom (SDF) strapdown gyroscope / |cby M.F. Vinnins and R. Apps.
264	1|aOttawa : |bDefence Research Establishment Ottawa, |cOctober 1984.
300	|a1 online resource (v, 28 pages) : |bcharts, illustrations
336	|atext|btxt|2rdacontent
337	|acomputer|bc|2rdamedia
338	|aonline resource|bcr|2rdacarrier
490	1 |aDREO technical note ; |vno. 85-2
500	|aDigitized edition from print [produced by Defence Research and Development Canada].
504	|aIncludes bibliographical references (page 26).
520	|a"Test results from the evaluation of a Honeywell GG1111 single-degree-of-freedom strapdown gyroscope are presented. Tests include both static and constant-rate tests in servo and in analog-torque-to-balance modes. Results of multi-position drift tests, drift stability, cool-down sensitivity, temperature sensitivity, torque generator linearity, scale factor stability and torque generator sensitivity to input axis rate changes are presented, described and discussed"--Abstract, page iii.
546	|aIncludes abstracts in English and French.
650	0|aGyroscopic instruments|xTesting.
650	6|aInstruments gyroscopiques|xEssais.
710	2 |aDefence Research Establishment Ottawa, |eissuing body.
710	1 |aCanada. |bDepartment of National Defence, |eissuing body.
830	#0|aDREO technical note ;|vno. 85-2.|w(CaOODSP)9.941800
856	40|qPDF|s858 KB|uhttps://publications.gc.ca/collections/collection_2024/rddc-drdc/DR52-18-43-1984-eng.pdf
986	|aPCN 32G01