Resumen
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.
Informaciones generales
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Estado: RetiradaFecha de publicación: 1992-06Etapa: Retirada de la Norma Internacional [95.99]
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Edición: 1Número de páginas: 8
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Comité Técnico :ISO/TC 20/SC 8
- RSS actualizaciones
Ciclo de vida
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Ahora
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Revisada por
PublicadoISO 1151-8:2022