. Magenta Areas: Unavailable
Terrain Information
The latitude range is - 90° to + 90°. When the aircraft flies to the North Pole, the latitude increases to 90°. When the aircraft passes the North Pole, the latitude decreases from 90° (vice versa across the South Pole). From a mathematical point of view, the latitude should increase when the aircraft flies to and passes the North Pole (i.e. …88°, 89°, 90°, 91°, 92°…). Due to the limits of the latitude range, the TAWS function considers there is no terrain information beyond 90° of latitude. The TAWS function displays the corresponding areas in magenta on ND (the amber TERR INOP indication is displayed on VD).
Note: EGPWS is also affected by these limitations. Refer to 4.1.5.5 – Terrain Display in Polar Areas.
7.1.4. WEATHER RADAR FUNCTION
The AESS Weather Radar function provides the same functions as conventional weather radars: weather detection with PWS and turbulence detection. The range goes up to 320 NM. The antenna scans an envelope of +/-80° in azimuth and +/- 15° in tilt. Refer to Figure 7-24.
The AESS Weather Radar function introduces a new concept: the weather radar does not directly display the weather information to the flight crew, but stores it in a 3D buffer. The 3D buffer significantly improves the weather analysis (i.e. on/off path weather, elevation mode, vertical view, Earth curvature correction, automatic ground mapping, weather displayed behind the aircraft) and the weather awareness.
Note: The weather radar basic principles remain identical to the ones described in 6 – Weather Surveillance –. Refer to this chapter for a refresher about weather radar physics.
7.1.4.1. WEATHER DETECTION
With weather returns stored in a 3D buffer, the AESS Weather Radar function provides different operating modes (automatic and manual). The following paragraphs describe the 3D buffer principles, and the automatic and manual operating modes.
7.1.4.1.1. 3D Buffer 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址:getting to grips with surveillance(110)