STATUS REPORT FOR PERIOD 1 JULY THROUGH 31 JULY 1970 U.S. GOVERNMENT CONTRACT (SANITIZED)

Document Type: 
Document Number (FOIA) /ESDN (CREST): 
CIA-RDP79B00873A001300010013-6
Release Decision: 
RIPPUB
Original Classification: 
K
Document Page Count: 
19
Document Creation Date: 
December 28, 2016
Document Release Date: 
August 29, 2012
Sequence Number: 
13
Case Number: 
Publication Date: 
July 1, 1970
Content Type: 
REPORT
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PDF icon CIA-RDP79B00873A001300010013-6.pdf641.33 KB
Body: 
Declassified in Part - Sanitized Copy Approved for Release 2012/08/29: CIA-RDP79B00873AO01300010013-6 Declassified in Part - Sanitized Copy Approved for Release 2012/08/29: CIA-RDP79B00873AO01300010013-6 Declassified in Part - Sanitized Copy Approved for Release 2012/08/29: CIA-RDP79B00873A001300010013-6 STATUS REPORT for period, 1. July through 31 July 1970 U.S. GOVERNMENT File No. 11038 STAT STAT _ Declassified in Part - Sanitized Copy Approved for Release 2012/08/29: CIA-RDP79B00873A001300010013-6 Declassified in Part - Sanitized Copy Approved for Release 2012/08/29: CIA-RDP79B00873AO01300010013-6 STAT Declassified in Part - Sanitized Copy Approved for Release 2012/08/29: CIA-RDP79B00873AO01300010013-6 Declassified in Part - Sanitized Copy Approved for Release 2012/08/29: CIA-RDP79B00873AO01300010013-6 The report period represented herein covers the period 1 July through 31 July 1970. Government Status Report under Contract to the U.S. This document is presented as the Monthly STAT STAT Project Manager STAT n Declassified in Part - Sanitized Copy Approved for Release 2012/08/29: CIA-RDP79B00873AO01300010013-6 M Declassified in Part - Sanitized Copy Approved for Release 2012/08/29: CIA-RDP79B00873A001300010013-6 fo INDEX Program Status Summary 1 Task 11: Stage Drives T11 :- Task 23: Optics Drive Assembly T23 - 1 through 9. Task 36: Overall Assembly T36 - I Task 43: Computer Programming T43 - 1 - Declassified in Part - Sanitized Copy Approved for Release 2012/08/29: CIA-RDP79B00873A001300010013-6 Declassified in Part - Sanitized Copy Approved for Release 2012/08/29: CIA-RDP79B00873A001300010013-6 PROGRAM STATUS SUMMARY Scheduled percentage of completion 97 % Actual percentage this date 90.6% The critical phase of installation and alignment of the optical system is essentially complete. It appears that so' far as the viewing branches of the optics and the main illumination systems are concerned, there has been no apparent damage in shipment and the performance is as anticipated. (This is based on. preliminary results only). The assembly work as a whole is on schedule and the results of the preliminary testing are very encouraging. M Declassified in Part - Sanitized Copy Approved for Release 2012/08/29: CIA-RDP79B00873A001300010013-6 Declassified in Part - Sanitized Copy Approved for Release 2012/08/29: CIA-RDP79B00873A001300010013-6 r STEREOCOMPARATOR TASK 11 STAGE DRIVES Scheduled percentage of completion 100% ?Actual percentage this date 96% E n The Stereocomparator stages exhibit a resonance of approximately The work during this report period involved instrumenting the stages with accelerometers and measuring the frequency of the resonance as various points of possible flexure were experimentally stiffened. The objective of this work is to isolate the 20 Hz resonance. Testing of the stage drives during this period was somewhat restricted due to the installation and alignment of the optical system. T11-1 Declassified in Part - Sanitized Copy Approved for Release 2012/08/29: CIA-RDP79B00873A001300010013-6 0 Declassified in Part - Sanitized Copy Approved for Release 2012/08/29: CIA-RDP79B00873AO01300010013-6 I El. . E, STEREOCOMPARATOR TASKS 16, 17, & 18 VIEWING. OPTICS, VIEWING ILLUMINATION, and RETICLE PROJECTOR and ILLUMINATION So'heduled percentage of completion 100% Actual percentage this date, 100% The optical installation and alignment has proceeded to the point where resolution tests have indicated values in white light of the order of 1,000 line pairs per millimeter at 200X magnification. In addition, stereo photographs have been placed in the Stereocom- parator and high quality stereo fusion has been readily achieved. T16,17 & 18 - 1 Declassified in Part - Sanitized Copy Approved for Release 2012/08/29: CIA-RDP79B00873AO01300010013-6 Declassified in Part - Sanitized Copy Approved for Release 2012/08/29: CIA-RDP79B00873A001300010013-6 STEREOCOM?ARATOR TASK 23 OPTICS DRIVE ASSEMBLY Scheduled percentage of completion 100% Actual percentage this date 98% Work on phasing.and servo .loop compensation for the Optics Drive systems is continuing. As explained in the previous re- port, in many systems. ' it has been found that current drive to the servo motors has yielded -greatly improved performance char- acteristics. The status of this work is as follows: A. Main Viewing Zoom It was found that the gear reduction system used in this system was difficult to couple electrically from a servo standpoint. The, system as originally ? constructed consisted of a high torque printed-cir- cuit motor followed by a PIC 80 to 1 gear reducer.. The output.shaft of this gear reducer was coupled through a further spur gear reduction to operate the barrel cam controlling the position of the lens ele- ments. It was found that the high torque output of the printed--circuit motor, when multiplied by the gear reduction ratio, was sufficient to -cause slippage of the spur gear mounted on the output shaft of the gear reducer. Declassified in Part - Sanitized Copy Approved for Release 2012/08/29: CIA-RDP79B00873A001300010013-6 Declassified in Part - Sanitized Copy Approved for Release 2012/08/29: CIA-RDP79B00873AO01300010013-6 In order to overcome this difficulty an experimental . setup was made which eliminated the use of the PIC gear reducer. In its place was substituted a straight 1/4" diameter shaft. The effect of removing the gear reducer was, of course, to reduce the motor operating speeds by a factor of 80. Additionally, the tachom- eter generator voltage is also reduced` by the same factor. The purpose of the experimental setup was to determine whether or not the system could be made to operate properly at such low speeds using very small tachometer feedback signals (full speed with this con- figuration gives a tachometer voltage of less than 0.1 volt). It was found that the system could be made to perform properly under these circumstances provided that the velocity feedback loop gain was increased by a large factor. This requirement- was due to the fact that the reflected inertia and friction loads on the motor shaft are quite high. The final configuration for this system gave a rate loop bandwidth of approximately 400 Hz and a position loop bandwidth of approximately 4.5 Hz. Rate loop control of the systems as is encountered in the manual operating mode was judged to be sufficiently T23-2 Declassified in Part - Sanitized Copy Approved for Release 2012/08/29: CIA-RDP79B00873AO01300010013-6 Declassified in Part - Sanitized Copy Approved for Release 2012/08/29: CIA-RDP79B00873A001300010013-6 r 1_i iJ n n smooth to provide satisfactory' viewing. characteristics. Only one difficulty remains with this system and that , lies in the fact that when the servo drive is not commanding the system, the mechanism. tends by gravity to preferentially seek the end limits of travel. In most of the systems in the Stereocomparator, a suf- ficient gear reduction exists such that the motor brush friction, when multiplied by the gear reduction ratio, is sufficient to hold the mechanical system in place under both power-off conditions and with. the rate loop only connected. With the- low gear reduction provision now installed in the viewing zooms, the motor brush friction "''torque does not get multiplied to a high enough value to prevent the load unbalance from driving the system back through - the -gear train. Means for leveling out the load characteristic over the range of travel of this assembly are being investigated, and it is expected that it will be possible to reduce the, load unbalance in the system to a sufficiently low value that the friction in the system can hold the mechanism in any selected location. B. Reticle lO X Zoom This system has been set up to follow the main viewing zoom in order to maintain a constant reticle pattern Declassified in Part - Sanitized Copy Approved for Release 2012/08/29: CIA-RDP79B00873A001300010013-6 Declassified in Part - Sanitized Copy Approved for Release 2012/08/29: CIA-RDP79B00873AO01300010013-6 size with varying magnification in the main optics. This system was found to have considerable back- lash present in the_ integral gear reducer package attached to the' motor/tachometer assembly, in order to achieve system stability, it was found nec- essary to reduce the position loop gain by a factor of 3; the rate loop gain was correspondingly increased to achieve' the- same steady-state resolution. Additionally, since this is a Type. Il system, containing two complex motor .integration poles, there is no velocity following error at constant speeds. The reduction of the. position loop gain has, however, increased the acceleration error characteristics for the system, and there is a noticeable.. delay, to responsd if the main viewing zoom is suddenly El accelerated. However, since under normal operating conditions the speeds and . accelerations present *in the optical systems are rather low, it has been found that the acceleration traoking errors present in this system 'produce no visible effects. Thus, the operating characteristics of the reticle zoom system appear to be satisfactory. Due to the sensitivity of the reticle projector system to - vibration,. no attempt has been made to measure the band- widthof the rate and position idops, but both appear adequate and the system is overdamped so that n6 overshoots or hunting is present. T23-4 Declassified in Part - Sanitized Copy Approved for Release 2012/08/29: CIA-RDP79B00873AO01360010013-6 r-? Declassified in Part - Sanitized Copy Approved for Release 2012/08/29: CIA-RDP79B00873AO01300010013-6 E C. Main Viewing Anamorph Ratio System This system has the compensation network designed and installed and the system appears to operate satisfactorily. The bandwidth of this system is somewhat less than the 4.5 Hz bandwidth attained in some of the other systems due to the fact that a very large gear reduction between the motor and the movable prisms exists. The motor there- fore has to reach very high velocities in order to cause significant motion of the prisms, and an acceleration limit is present in the system since the servo-amplifier has a voltage limit. Additionally, in order to secure suffi- cient feedback potentiometer travel from the small angular motions. 'of the anamorph prisms, a precision step-up gearir}g arrangement is used between the prism pinions and the potentiometer shaft. A small amount of backlash is present in this. system and it was found that a wideband system displayed an.unstable limit cycle caused by both this back-. lash and the backlash present in the gear.reducer which is integrally mounted to the motor/tachometer assembly. Reduction of.. the rate loop bandwidth and the use of the current. Source servo-amplifiers described previously yielded a stable system which has good transient characteristics (overdarnped). It is expected that the operation of this system as configured is satisfactory for use in the T23-5 Declassified in Part - Sanitized Copy Approved for Release 2012/08/29: CIA-RDP79B00873AO01300010013-6 G Declassified in Part - Sanitized Copy Approved for Release 2012/08/29: CIA-RDP79B00873A001300010013-6 Stereocomparator because the anamorph optical function itself is not as drastic to the operator's eyes as are the parallax and image rotation functions. D. Reticle Anamorph Ratio System The reticle anamorph ratio system is mechanically similar to the main viewing anamorph ratio assembly, but of much smaller and lighter construction. Since virtually all of the optics drives systems, with the exception of the main viewing zoom, are instrument-type servo loops (i.e., the load mass reflected to the motor is insignificant com- pared to the inertia of the motor itself) a compensation network similar to that used on the main viewing anamorph system was installed on the reticle anamorph ratio sub- assembly. Operation of this system appeared to be similar to that.of the main anamorph system except' that it was found possible to increase the bandwidth of the system by approximately 25% in order to minimize following errors. Satisfactory results were obtained with this configuration. The reticle anamorph system was found to have some diffi- culties associated'with the limit switch system; specifically the prelimits, which command a velocity slowdown as the limit of travel is approached, have an operating point which extends a great distance into the active operating area P .123-6 Declassified in Part - Sanitized Copy Approved for Release 2012/08/29: CIA-RDP79B00873A001300010013-6 Declassified in Part - Sanitized Copy Approved for Release 2012/08/29: CIA-RDP79B00873AO01300010013-6 rl L j n L) of the range of travel of the system. The result is that if the main anamorph is slewed rapidly there is an appre- ciable lag in the reticle anamorph system response due to the velocity of the reticle anamorph being limited to approximately 10%of full speed over most of its, range. The operator therefore could see the reticle spot become elongated for a brief period of time until the reticle ana- morph system catches up the main anamorph, at which time the reticle spot becomes round. Since during normal measuring operations, the optical elements are generally moving quite slowly, it is expected that this characteristic will not .produce any troublesome effects. The limit switch arrangement in this system also has a difficulty that apses from the fact that the actuating cam motions-, are very small, and there is some hysteresis in the microswitch. This situation precludes the use of an int.6grator in the. rate loop for the system, because once alimit of travel is reached, further velocity commands in the direction" of the limit are not permitted to pass into the system. (This is effected by means of blocking diodes on the velocity input to the servo). With an integrator in the system even though the' input has no command applied, miscellaneous bias and offset currents are present and will cause the integrator to drift. (The position loop is T23-7 Declassified in Part - Sanitized Copy Approved for Release 2012/08/29: CIA-RDP79B00873AO01300010013-6 - Declassified in Part - Sanitized Copy Approved for Release 2012/08/29: CIA-RDP79B00873AO01300010013-6 opened by the blocking diode). Thus this particular system could drift of its own accord into the second limit micro- switch actuation point which would require activation of the second limit bypass circuitry in order to pull the system back into its. operating range. It was therefore decided that a non-integrating (Type I) loop configuration would be used. This type of system has a finite, although small, velocity following error, but this small error is not noticeable to the operator even at very high anamorph ratios. E . 4X - Reticle Site Zoom This relay operated system is under manual control of the operator and allows him to set the diameter of the reticle spot in each eyepiece to a convenient size for viewing. Two speeds of operation in each direction are provided. This system operates in a satisfactory manner.- F. Reticle Brightness Control System This system consists of a pair of counter-rotating variable- density filter wheels placed in the reticle optical path to control the apparent brightness of the reticle spot. The system, has been connected to the relay control system and operates entirely satisfactorily, giving two speeds in each. direction of operation. Declassified in Part - Sanitized Copy Approved for Release 2012/08/29: CIA-RDP79B00873AO01300010013-6 Declassified in Part - Sanitized Copy Approved for Release 2012/08/29: CIA-RDP79B00873AO01300010013-6 2 :11 G. Illumination Condenser Permutation Systems When changing from the low range to the high range of magnification-in the Stereocomparator, it is necessary to switch three optical assemblies in the illumination system. These consist of a large afocal condenser lens assembly; and reorientation of the outer ring of the variable beam-defining iris located below the illumination condenser zoom assembly. These changeover systems are operated by means of geneva drive mechanisms. An exception is the iris changeover which utilizes a slip clutch to allow overtravel of the motor pinion. These systems have been connected to the relay control unit, and it is found that the changeover occurs in approximately six seconds. As has been mentioned in previous reports, it is necessary to drive the variable beam-defining iris systems to a pre- determined location before changeover can occur. Depending on the setting of the main viewing zoom, this motion could take as long as three seconds. After the permutation change- over has occurred, the variable iris must then slew to the proper point corresponding to the new zoom setting which could also take as long as three seconds. Thus it can be seen that a complete changeover sequence from one magnification range to the other will require a maximum of 12 seconds. These systems work satisfactorily. T23-9,- Declassified in Part - Sanitized Copy Approved for Release 2012/08/29: CIA-RDP79B00873AO01300010013-6 Declassified in Part - Sanitized Copy Approved for Release 2012/08/29: CIA-RDP79B00873AO01300010013-6 M n STEREOCO MPARATOR TASK 36 OVERALL ASSEMBLY Scheduled percentage of completion 100% n Actual percentage this date 90% During this report period the optical subassemblies received from the optical subcontractor were assembled into the Stereo- comparator: The optical alignment has now proceeded to the point where resolution tests have indicated values in white light of the order of 1,000 line pairs per millimeter at 200X magnif ication . In addition, stereo photographs have been placed in the Stereocomparator and high quality stereo fusion has.been readily achieved. The main viewing branch on the right side optics appeared generally satisfactory, based on preliminary tests. The left side optics exhibited difficulties with image wander. This necessitated the performance of additional' alignment procedures. obtained from the optical subcontractor. This realignment work is presently almost complete, with good results being achieved. T36 - 1 Declassified in Part - Sanitized Copy Approved for Release 2012/08/29: CIA-RDP79B00873AO01300010013-6 Declassified in Part - Sanitized Copy Approved for Release 2012/08/29: CIA-RDP79B00873AO01300010013-6 STEREOCOMPARATOR COMPUTER PROGRAMMING AND SERVICES Scheduled percentage of completion 100% Actual, percentage this date 93% E Recoding of the teletype data input package of subroutines to incor- porate real formats and real units (see Status Report for June, Task 43) was completed. The information available on the formats desired for the pan and strip systems was believed to be accurate and complete. The information available for the frame system was somewhat less so, but was utilized as well as possible. The lists of items used in normal operation include a number of items which are not actually required for the Honeywell computer. These were included in order to keep the lists standard. They can be readily deleted if they turn out to be undesirable. Provision was incorporated both for punching paper tape simultaneously with typing the requested information and for reading from a paper tape if one is available. Both of these features are optional to the operator. During the next several weeks) will be doing such recoding of the computer program as is required to utilize the additional 16K core memory which has been added to the Honeywell computer. Other- wise Task 43 is completed, except for the final system integration. STAT Declassified in Part - Sanitized Copy Approved for Release 2012/08/29: CIA-RDP79B00873AO01300010013-6