Cockpit de vidro (Glass Cockpit) (Glass Cockpit)
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Definition
Cabine de comando com grandes displays eletrônicos multifuncionais substituindo os instrumentos analógicos tradicionais.
O que é um glass cockpit?
A glass cockpit is a flight deck in which traditional electromechanical analog flight instruments — the altimeter, airspeed indicator, attitude indicator, vertical speed indicator, heading indicator, and navigation displays — are replaced by large multifunction liquid crystal or OLED screens. These displays can reconfigure to show any combination of flight data, system synoptics, moving maps, weather radar overlays, and traffic information, dramatically reducing cockpit clutter and pilot workload.
Como funciona
The core of a glass cockpit is the Primary Flight Display (PFD) and Navigation Display (ND) — or a combined Electronic Flight Instrument System (EFIS). Data flows from:
- Air Data Computers (ADC): Airspeed, altitude, vertical speed, Mach number from pitot-static system
- Inertial Reference Systems (IRS): Attitude, heading, acceleration, ground speed
- GPS/FMS: Position and flight plan data overlaid on the moving map ND
- Engine/systems data: Displayed on Engine Indicating and Crew Alerting System (EICAS) or Electronic Centralized Aircraft Monitoring (ECAM) displays
The PFD integrates what once required six separate instruments into a single intuitive display. The ND overlays flight plan route, weather radar returns, TCAS traffic, and terrain. Pilots interact with display modes through dedicated control panels. Integration with the FMS and autopilot provides a fully coupled flight management environment, and a HUD can mirror PFD data into the pilot's forward view.
Evolução e sistemas modernos
The Boeing 767 (1982) and Airbus A310 introduced early EFIS displays. The Airbus A320 (1988) introduced a full glass cockpit with sidestick and fly-by-wire. The Boeing 777 (1995) brought the world's first fully digital, triple-redundant glass cockpit. Today's A350 and 787 feature large-format displays (up to 15 inches), touchscreen CDUs, and synthetic vision systems that display terrain and runway in 3D even in zero-visibility conditions. General aviation glass cockpits — Garmin G1000, Avidyne Entegra — have become standard in new training and personal aircraft.
Requisitos regulatórios
Display systems must meet RTCA DO-178C (software) and DO-254 (hardware) standards. Minimum display performance standards are specified in FAA TSO-C113b and EASA ETSO-C113b. Redundancy is required: at least one standby attitude indicator (often an ISIS — Integrated Standby Instrument System) must remain operational on battery power if all electronic displays fail. Type certification requires demonstration of readability under all lighting conditions including direct sunlight.
Related Terms
Barramento Elétrico
Uma rede de distribuição de energia dentro de uma aeronave que direciona energia elétrica de geradores, APU ou baterias para a aviônica e sistemas, organizada em níveis de prioridade para garantir que os equipamentos críticos recebam energia primeiro.
Cockpit
A seção da aeronave onde os pilotos controlam o avião, abrigando instrumentos e comandos de voo.
Fly-By-Light
Um sistema avançado de controle de voo que usa cabos de fibra óptica em vez de fios elétricos para transmitir sinais de controle, oferecendo imunidade a interferências eletromagnéticas.
Revolução Fly-by-Wire
A transformação dos sistemas de controle de aeronaves de cabos mecânicos e hidráulicos para computadores digitais eletrônicos, liderada comercialmente pelo Airbus A320, que entrou em serviço em 1988.