Standard

ISO 1151-1:1988

Apr 1988 Current

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Abstract

Gives basic definitions and deals with motion relative to the atmosphere, assumed to be at rest or in translational motion at constant velocity relative to the Earth. The aircraft is assumed to be rigid. However, most of the definitions can be applied to the case of a flexible aircraft. Describes axis systems, angles, velocities and angular velocities, aircraft inertia, forces, moments, coefficients and load factors, thrust, resultant moment of propulsive force, coefficients thereof, control forces and moments, motivators and their forces and moments.

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Standard from ISO
Published: April 28 1988
Edition: 4
Document type: IS
Pages
ISBN:

Publisher: ISO
Distributor: ISO
ICS: 01.060
ICS: 49.020
International TC: ISO/TC 20/SC 8

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Revises: ISO 1151-1:1985
Revises: ISO 1151:1972

ISO 1151-1:1988

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ISO 1151-1:1988

ISO 1151-1:1985

ISO 1151-1:1975

ISO 1151:1972

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Version history History (4)

ISO 1151-1:1988

ISO 1151-1:1985

ISO 1151-1:1975

ISO 1151:1972

Abstract

Products specifications

Product Relations

Product life cycle