3. Design principles for non-vibrating accelerometers
The number of EM/B degrees of freedom may be one (by far the most common case), two or three (in the case of CACTUS,
4.6
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Design principles for non-vibrating accelerometers
Bibliography
Works
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(1) - McLAREN (I.) -
Open and closed loop accelerometers.
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AGARD flight test instrumentation series AGARDograph 160 Vol. 6 39 p. bibl. 19 réf. 1974 AGARD.
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(2) - RADIX (J.-C.) -
Systèmes inertiels à composants liés " strap-down ".
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