Abstract Preview
The aircraft is assumed to be rigid, of constant mass and of constant inertia. It is not equipped with systems modifying its natural dynamic behaviour. However, most of the definitions can be applied to the case of a flexible aircraft, of variable mass and of variable inertia. The general concepts defined are applicable to the atmospheric flight phase.
General information
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Status : PublishedPublication date : 1992-06
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Edition : 1Number of pages : 8
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- ICS :
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Quantities and units
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Aircraft and space vehicles in general
Buy this standard
| Format | Language | |
|---|---|---|
| Paper |
- CHF58
Life cycle
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