ISO-1151-8 › Historical Revision Information
Flight dynamics - Concepts, quantities and symbols - Part 8: Concepts and quantities used in the study of the dynamic behaviour of the aircraft
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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.
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Document Number
ISO 1151-8:1992
Revision Level
1ST EDITION
Status
Superseded
Publication Date
June 15, 1992
Committee Number
ISO TC 20/SC 3