LEADER 01807nam 2200373 450 001 9910135477803321 005 20231208090800.0 010 $a0-7381-0547-3 024 7 $a10.1109/IEEESTD.1981.81058 035 $a(CKB)3780000000092985 035 $a(NjHacI)993780000000092985 035 $a(EXLCZ)993780000000092985 100 $a20231208d1981 uy 0 101 0 $aeng 135 $aur||||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aIEEE Std 529-1980 $esupplement for strapdown applications to IEEE standard specification format guide and test procedure for single-degree-of-freedom rate-integrating gyros /$fIEEE 210 1$a[Place of publication not identified] :$cIEEE,$d1981. 215 $a1 online resource 330 $aA specification format guide for the preparation of a rate-integrating gyroscope specification is presented. Recommended procedures for testing a rate-integrating gyroscope are compiled. This standard, when combined with IEEE Std 517-1974 (R1980), defines the requirements and test procedures in terms of characteristics unique to the gyroscope or those applications in which the dynamic angular inputs are significantly greater than the limitations identified in IEEE Std 517. 517 $aIEEE Std 529-1980: Supplement for Strapdown Applications to IEEE Standard Specification Format Guide and Test Procedure for Single-Degree-of-Freedom Rate-Integrating Gyros 606 $aSpace vehicles$xTesting 606 $aAerospace engineering 615 0$aSpace vehicles$xTesting. 615 0$aAerospace engineering. 676 $a629.454 801 0$bNjHacI 801 1$bNjHacl 906 $aDOCUMENT 912 $a9910135477803321 996 $aIEEE Std 529-1980$92577540 997 $aUNINA