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060911s1975 gr r f000 0 eng d |
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|a GR-KoDPT
|b gre
|e AACR2
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| 100 |
1 |
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|a Sherman, Windsor L.
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| 245 |
1 |
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|a Effect of external disturbances and data rate on the response of an automatic landing system capable of curved trajectories/
|c Windsor L. Sherman ; Langley Research Center
|
| 260 |
|
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|a Washington, D.C.:
|b National Aeronautics and Space Administration,
|c 1975
|
| 300 |
|
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|a 45 σ. :
|b εικ. ;
|c 27 εκ.
|
| 490 |
0 |
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|a NASA technical note
|v D-7971
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| 504 |
|
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|a Βιβλιογραφία: σ. 21
|
| 650 |
|
0 |
|a Guidance systems (Flight)
|
| 650 |
|
0 |
|a Airplanes
|x Landing
|
| 710 |
|
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|a United States
|b National Aeronautics and Space Administration
|x Equipment and supplies
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| 710 |
2 |
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|a Langley Research Center
|
| 710 |
0 |
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|a United States.
|b National Aeronautics and Space Administration
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| 952 |
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|a GR-KoDPT
|b 59cc2d706c5ad13446fa7caa
|c 998a
|d 945l
|e TL 521 .3
|t 1
|x m
|z Books
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