<< attitude indicator | augmentation system | authorized agent >>
Back to: "A"
augmentation system
- Fonte1
- INTERNATIONAL CIVIL AVIATION ORGANIZATION. National plan for CNS/ATM systems: guidance material. Montreal, 2000. (Cir. 278 AN/164).
- Fonte2
- INTERNATIONAL CIVIL AVIATION ORGANIZATION. Manual of aircraft accident and incident investigation. Part III: investigation. Montreal, 2011. (Doc. 9756 AN/965).
- Fonte3
- AGÊNCIA NACIONAL DE AVIAÇÃO CIVIL (Brasil). Instrução Suplementar n. 21-013, de 16 de agosto de 2012. Instruções para obtenção de aprovação de instalação de equipamentos GNSS (Global Navigation Satellite Systems) stand alone para operações VFR e IFR PBN (Performance-Based Navigation.
- Contexto
- Other risk areas are expected to be mitigated as GNSS continues to evolve to a more comprehensive service that will include the introduction of additional signals for aeronautical use on GPS and GLONASS satellites, augmentation system improvements, and the introduction of additional satellites and satellite systems. Each State will have to evaluate the effectiveness of the mitigation techniques applied in its airspace to determine when it is acceptable to rely on GNSS alone for the provision of navigation service.
- The state of the art fly-by-wire flight control system is a quadruplex command and stability augmentation system. It employs a fly-by-wire concept. The pilot-initiated control inputs are transmitted via quadrex electrical signals rather than mechanical linkage. The wiring is separated by branches. There are two to four branches down each side of the aircraft to prevent loss of the system to damage in one area.
- Français
- renforcement