avionics displays cp

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Avionics displays EFIS DA _ CP M S Prasad

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Page 1: Avionics Displays CP

Avionics displays EFIS

DA _ CP M S Prasad

Page 2: Avionics Displays CP

• Primary flight information,• Navigation information,• Engine data,• Airframe data,• Warning information.

• Infrared imaging sensors,• Radar,• Tactical mission data,• Weapon aiming,• Threat warnings.

• Head up displays,• Helmet mounted displays,• Multi-function color displays,• Digitally generated color moving map displays,

DISPLAYS

Page 3: Avionics Displays CP

Primary display

displaying aircraft attitude and flight control system steering commands including VOR, localizer, TACAN, or RNAV deviation; and glide slope or pre-selected altitude deviation. The PFD provides flight control system mode annunciation, auto-pilot engage annunciation, attitude source annunciation, marker beacon annunciation, radar altitude, decision height set and annunciation, fast-slow deviation or angle-altitude alert, and excessive ILS deviation.

Page 4: Avionics Displays CP
Page 5: Avionics Displays CP

HUD Sample display

The Navigation Display (ND) : provides a plan view of the aircraft’s horizontal navigation situation. Data includes heading and track, VOR, ILS, or RNAV course and deviation, navigation source annunciation, to/from, distance/direction, time-to-go, elapsed time, course information and source annunciation from a second navigation source, and weather radar data. f the

Page 6: Avionics Displays CP

1. Inherent advantages of Head-up presentation of primary flight information including depiction of the aircraft’s flight path vector, resulting in improved situational awareness and increased safety in circumstances such as wind shear or terrain/traffic avoidance maneuvers.

2. To display automatic landing guidance to enable the pilot to land the aircraft safely in conditions of very low visibility due to fog, as a back up and monitor for the automatic landing system. The display of taxi-way guidance is also being considered.3. Enhanced vision using a raster mode HUD to project a FLIR video picture of the outside world from a FLIR sensor installed in the aircraft,.

IFOV = 2 tan ^-1 D/2L whr D = dia of collimating lens and L distance of eye from lens.

TFOV Total field which observer can see by moving is eyes.

The instantaneous field of view is the angular coverage of the imagery which canBe seen by the observer at any specific instant

Page 7: Avionics Displays CP

Refractive Optics

Reflective Optics

Page 8: Avionics Displays CP

Basic Principle HUD

Page 9: Avionics Displays CP

Binocular HMD and Virtual Cockpit

Page 10: Avionics Displays CP

Primary flight display

Engine Display