Résumé
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.
Informations générales
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État actuel: AnnuléeDate de publication: 1992-06Stade: Annulation de la Norme internationale [95.99]
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Edition: 1Nombre de pages: 8
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Comité technique :ISO/TC 20/SC 8
- RSS mises à jour
Cycle de vie
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Actuellement
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Révisée par
PubliéeISO 1151-8:2022