If you wish to contribute or participate in the discussions about articles you are invited to join SKYbrary as a registered user
Radio Altimeter
From SKYbrary Wiki
| Article Information | ||
|---|---|---|
| Category: | Flight Technical | |
| Content source: | SKYbrary | |
| Content control: | EUROCONTROL | |
Contents |
Definition
A radio altimeter is an airborne electronic device capable of measuring the height of the aircraft above terrain immediately below the aircraft.
Description
Early radio altimeters determined altitude by measuring the time between transmission of a radio signal from the aircraft and reception of the reflected signal. Modern systems use other means, for example, measurement of the change of phase between transmitted and reflected signal.
The radio altimeter commences operation when the aircraft descends below 2500 ft above ground level, and this is indicated visually (e.g. by dissapearance of an 'OFF' flag and emergence of the altitude needle from behind a mask).
Radio altimeter calls may be either:
- Announced by the PNF; or,
- Generated automatically by a synthesized voice.
The rate of change of phase of the radio signal is proportional to the rate of climb or descent, and this is used along with the radio altitude as an essential input to ground proximity warning systems.
Use of the radio altimeter is integral to Low Visibility Operations, where it is used to determine when the aircraft reaches decision height.
Prudent use of the radio altimeter is also a valuable defence against CFIT.
Related Articles
Further Reading
- IR-OPS SPA.LVO.110&120 deals with Low Visibility Operations
- See also Acceptable Means of Compliance and Guidance Material to IR-OPS SPA.LVO.110&120
- EU-OPS 1.440 and Appendices to EU-OPS 1.440 and EU-OPS 1.450 deal with Low Visibility Operations.