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.
Status: WithdrawnPublication date: 1992-06
Edition: 1Number of pages: 8
Technical Committee: ISO/TC 20/SC 8 Aerospace terminology
This standard contributes to the following Sustainable Development Goal:
ISO 1151-8:1992Stage: 95.99
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