ISO 1151-8:1992

This standard has been revised by ISO 1151-8:2022

Abstract

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

Status
: Withdrawn

Publication date
: 1992-06

Stage
: Withdrawal of International Standard [95.99]
Edition
: 1

Number of pages
: 8
Technical Committee :
ISO/TC 20/SC 8

ICS :
01.060 49.020
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