25 hits 24.62 per million (hits/wds×1,000,000), 34.59/mill in RefCorp for KEYNESS=0.71 in brown_strip.txt [?]
001. , EQU (Equate), CODE, DTF (Define Tape File), DIOCS (Define INPUT /Output Control System), and DUF (Descriptive Entry for
002. ined in the 7070 Data Processing system Bulletin " IBM 7070 INPUT /Output Control System", form J28-6033-1. Brief descrip
003. noticed in Fig. 7-1 that the accelerometer responds to any INPUT acceleration. The equation relating input acceleration
004. ocoder declarative statements follow below. _ DIOCS- DEFINE INPUT /OUTPUT CONTROL SYSTEM_ When the Input/Output Control S
005. changing the foil area and adjusting the electrical energy INPUT to the foil. MEASUREMENTS OF INTERSTELLAR
006. ture research tools often more than 50% of the total energy INPUT is being transferred to the co0ling medium of the anod
007. the servo loop gain. In addition, the cutoff frequency for INPUT accelerations is approximately proportional to the ser
008. eful choice of photocathode which maximizes **f for a given INPUT E (in the case of the second stage, for the first phos
009. h the gyro is controlling. This is normally termed the gyro INPUT axis, 90` away from the gyro output or|j axis. The gy
010. of photocathodes ( S-11 and S-20) and three types of light INPUT. The input light distributions considered are P-11 and
011. 1 and P-20 phosphor screens, for night light and P-20 light INPUT. (The P-20 input is of interest because it corresponds
012. ffect of device and quantum noise, associated with such low INPUT levels, will be described. After these theoretical con
013. or screens, for night light and P-20 light input. (The P-20 INPUT is of interest because it corresponds roughly to the l
014. r responds to any input acceleration. The equation relating INPUT acceleration to output platform angle is **f In practi
015. e accelerometer is properly aligned, the other is also. The INPUT axis of the appropriate gyros are parallel to the sens
016. elow. _ DIOCS- DEFINE INPUT/OUTPUT CONTROL SYSTEM_ When the INPUT /Output Control System is to be used in a program, a DI
017. IOCS, DTF, and DUF statements are used when required by the INPUT /Output Control System. DIOCS is used to select the maj
018. o direct the platform into proper heading. In Fig. 7-4, the INPUT axis of the three-axis platform is shown at some point
019. ro input axis is parallel to the north-south direction. The INPUT axis of the X gyro, when pointing in the east-west dir
020. slation after glossary lookup is structural analysis of the INPUT text. The grammatical description of each occurrence i
021. thodes ( S-11 and S-20) and three types of light input. The INPUT light distributions considered are P-11 and P-20 phosp
022. uminous flux gain of a single stage is given by: **f If the INPUT light distribution falls beyond the visible range, **f
023. f earth. If the platform is not properly headed, the X-gyro INPUT axis will see a component of the earth's rotation. The
024. platform is leveled and properly headed, so that the X-gyro INPUT axis is parallel to the east-west direction and the Y-
025. axis is parallel to the east-west direction and the Y-gyro INPUT axis is parallel to the north-south direction. The inp