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| 001 | 102857465 | ||
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| 035 | ⊔ | ⊔ | ‡a(MiU)99187539616706381 |
| 035 | ⊔ | ⊔ | ‡asdr-miu.99187539616706381 |
| 035 | ⊔ | ⊔ | ‡a(OCoLC)417700187 |
| 035 | ⊔ | ⊔ | ‡a(GWLA)gwla ocn417700187 |
| 040 | ⊔ | ⊔ | ‡aLHL ‡beng ‡cLHL ‡dOCLCQ ‡dOCLCF ‡dOCLCO ‡dOCLCQ ‡dOCLCA ‡dTRAAL |
| 049 | ⊔ | ⊔ | ‡aMAIN |
| 086 | 0 | ⊔ | ‡aD 301.45/46-2:70-102 |
| 088 | ⊔ | ⊔ | ‡aAD 0722773 |
| 088 | ⊔ | ⊔ | ‡aAFFDL TR 70-102 |
| 100 | 1 | ⊔ | ‡aGraham, Dunstan, ‡eauthor. |
| 245 | 1 | 0 | ‡aInvestigation of measuring system requirements for instrument low visibility approach / ‡cDunstan Graham, Warren F. Clement, Lee Gregor Hofmann. |
| 264 | ⊔ | 1 | ‡aWright-Patterson AFB, Ohio : ‡bAir Force Flight Dynamics Laboratory, Aeronautical Systems Division, United States Air Force, ‡c1971. |
| 300 | ⊔ | ⊔ | ‡axxix, 185 pages : ‡billustrations ; ‡c28 cm. |
| 336 | ⊔ | ⊔ | ‡atext ‡btxt ‡2rdacontent |
| 337 | ⊔ | ⊔ | ‡aunmediated ‡bn ‡2rdamedia |
| 338 | ⊔ | ⊔ | ‡avolume ‡bnc ‡2rdacarrier |
| 490 | 0 | ⊔ | ‡aAir Force Flight Dynamics Laboratory (U.S.). Technical report ; ‡vAFFDL TR 70-102 |
| 500 | ⊔ | ⊔ | ‡aAD0722773 (from http://www.dtic.mil). |
| 500 | ⊔ | ⊔ | ‡a"February 1971." |
| 504 | ⊔ | ⊔ | ‡aIncludes bibliographical references (pages 135-138). |
| 520 | ⊔ | ⊔ | ‡aA practical method of determining measuring system requirements for instrument low visibility approach is presented. The method is made to depend on system analysis of the airplane, its control system, and the guidance system, as well as on atmospheric turbulence inputs and radio guidance system fluctuation noise. Requirements on the system are set in terms of a low value of the accident exposure multiplier which is related to the probability of a missed approach in the assumed environment. The application of the method is demonstrated in connection with two examples: manual-flight director approach in the A-7D attack airplane, and automatically coupled approach with an advanced 'windproof' flight control system in the DC-8 transport aircraft. The results, including particularly the implied requirements on scan rate for a scanning beam instrument low visibility approach system, demonstrate the interconnections between scanning rate, flight control, and overall system performance. |
| 536 | ⊔ | ⊔ | ‡aResearch supported by the Air Force Flight Dynamics Laboratory, Aeronautical Systems Division, United States Air Force, and performed by Systems Technology, Inc., Hawthorne, California, under contract no. ‡bF33615-69-C-1904. |
| 538 | ⊔ | ⊔ | ‡aMode of access: Internet. |
| 650 | ⊔ | 7 | ‡aLanding aids (Aeronautics) ‡2fast ‡0(OCoLC)fst00991698 |
| 650 | ⊔ | 7 | ‡aInstrument landing systems. ‡2fast ‡0(OCoLC)fst00974385 |
| 650 | ⊔ | 7 | ‡aAirplanes ‡xLanding. ‡2fast ‡0(OCoLC)fst00803254 |
| 650 | ⊔ | 7 | ‡aAirplanes ‡xControl systems. ‡2fast ‡0(OCoLC)fst00803111 |
| 650 | ⊔ | 0 | ‡aLanding aids (Aeronautics) |
| 650 | ⊔ | 0 | ‡aInstrument landing systems. |
| 650 | ⊔ | 0 | ‡aAirplanes ‡xControl systems. |
| 650 | ⊔ | 0 | ‡aAirplanes ‡xLanding. |
| 700 | 1 | ⊔ | ‡aHofmann, Lee Gregor, ‡eauthor. |
| 700 | 1 | ⊔ | ‡aClement, Warren F., ‡eauthor. |
| 710 | 2 | ⊔ | ‡aAir Force Flight Dynamics Laboratory (U.S.), ‡esponsor. |
| 710 | 1 | ⊔ | ‡aUnited States. ‡bAir Force. ‡bSystems Command, ‡eissuing body. |
| 710 | 2 | ⊔ | ‡aSystems Technology, Inc., ‡esponsor. |
| 730 | 0 | ⊔ | ‡aTechnical Report Archive & Image Library (TRAIL) |
| 899 | ⊔ | ⊔ | ‡a39015095318864 |
| CID | ⊔ | ⊔ | ‡a102857465 |
| DAT | 0 | ⊔ | ‡a20210401082116.0 ‡b20220412000000.0 |
| DAT | 1 | ⊔ | ‡a20220412060511.0 ‡b2024-02-14T18:41:13Z |
| CAT | ⊔ | ⊔ | ‡aSDR-MIU ‡dALMA ‡lprepare.pl-004-008 |
| FMT | ⊔ | ⊔ | ‡aBK |
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| 974 | ⊔ | ⊔ | ‡bMIU ‡cGWLA ‡d20240214 ‡sgoogle ‡umdp.39015095318864 ‡y1971 ‡rpd ‡qbib ‡tUS fed doc |