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inertial navigation system
- Definição1
- A computer-based navigation system that tracks the movement of an aircraft via signals produced by onboard accelerometers. The initialG-16 location of the aircraft is entered into the computer, and all subsequent movement of the aircraft is sensed and used to keep the position updated. An INS does not require any inputs from outside signals.
- Fonte1
- FEDERAL AVIATION ADMINISTRATION. Pilot's handbook of aeronautical knowledge. [s.l.], 2008. Disponível em http:// www.faa.gov/regulations_policies/handbooks_manuals /aviation/pilot_handbook/media/PHAK %20-%20Cover-Preface.pdf. Acesso em: 20 fev.2015.
- Fonte2
- INTERNATIONAL CIVIL AVIATION ORGANIZATION. Manual on testing of radio navigation aids. Fourth edition. Montreal, 2000. (Doc. 8071)
- Nota adicional1
- Acronym in English: INS.
- Contexto
- If the flight check aircraft is fitted with a Doppler or inertial navigation system, it can of course be used to measure the coverage area.
- Subárea1
- Air Navigation Aids
- Português
- sistema de navegação inercial