Conventional reference sensors are impractical at altitudes and velocities of planned X-15 flight path; inertial reference system used, which includes transistorized integrator amplifier with gain of 1/4 million is described.
Guidance systems in manned space flight
Electronics
Electronics ; 32 , n 33
1959
3 pages
Aufsatz (Zeitschrift)
Englisch
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NTRS | 1962
|Systems engineering, manned space flight.
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|Engineering Index Backfile | 1963
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