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stability augmentation system
- Definição1
- An auxiliary system to the basic manual vehicle control system whereby response of the control surfaces to inputs by the pilot can be adjusted to give a pre-selected vehicle response by selection of certain fixed gains in a standard feedback loop on control-surface output.
- Fonte1
- MULTILINGUAL aeronautical dictionary, or, dictionary aeronautique multilingue: english, french, spanish, dutch, greek, italian,portuguese, turkish. London, England: Technical Editing and reproduction Ltd, 1980. xx, 876 p. ISBN 92835016667
- Fonte2
- INTERNATIONAL CIVIL AVIATION ORGANIZATION. Annex 8 to the Convention on International Civil Aviation. Airworthiness of aircraft. 11th ed. Montreal, 2010.
- Contexto
- The aeroplane shall have such stability in relation to its other flight characteristics, performance, structural strength, and most probable operating conditions (e.g. aeroplane configurations and speed ranges) as to ensure that demands made on the pilot’s powers of concentration are not excessive when the stage of the flight at which these demands occur and their duration are taken into account. The stability of the aeroplane shall not, however, be such that excessive demands are made on the pilot’s strength or that the safety of the aeroplane is prejudiced by lack of manoeuvrability in emergency conditions. It shall be shown that any combination of failures or conditions that would result in the need for exceptional piloting skills is extremely improbable. The stability may be achieved by natural or artificial means, or a combination of both. If compliance with the flight characteristics requirements is dependent upon a stability augmentation system or upon any other automatic or power-operated system, compliance shall be shown with 4.2 of this part.
- Subárea
- Air Navigation
- Français
- système d’augmentation de stabilité