Any device which measures the height of an aircraft. The two chief types are the pressure altimeter, which measures the aircraft's distance above sea level, and the radar altimeter, which measures distance above the ground.
Pressure altimeter
A pressure altimeter precisely measures the pressure of the air at the level an aircraft is flying and converts the pressure measurement to an indication of height above sea level according to a standard pressure-altitude relationship. In essence, a pressure altimeter is a highly refined aneroid barometer since it utilizes an evacuated capsule whose movement or force is directly related to the pressure on the outside of the capsule. Various methods are used to sense the capsule function and cause a display to respond such that the pilot sees the altitude level much as one looks at a watch.
Because altitude measured in this manner is also subject to changes in local barometric pressure, altimeters are provided with a barosetting that allows the pilot to compensate for these weather changes, the sea-level air pressure to which the altimeter is adjusted appearing in a window of the dial. Flights below 18,000 ft (5486 m) must constantly contact the nearest traffic center to keep the altimeters so updated. Flights above 18,000 ft and over international waters utilize a constant altimeter setting of 29.92 in. Hg, or 1013.2 millibars (101.32 kilopascals), so that all high-flying aircraft have the same reference and will be interrelated, providing an extra margin of safety. See also Air navigation.
Radar altimeter
A radar altimeter is a low-power radar that measures the distance of an aircraft (or other aerospace vehicle) above the ground. Radar altimeters are often used in aircraft during bad-weather landings. They are an essential part of many blind-landing and automatic navigation systems and are used over mountains to indicate terrain clearance. Special types are used in surveying for quick determination of profiles. Radar altimeters are used in bombs, missiles, and shells as proximity fuses to cause detonation or to initiate other functions at set altitudes. Radar altimeters have been used on various spacecraft, starting with Skylab in 1973, to measure the shape of the geoid and heights of waves and tides over the oceans. Other spacecraft altimeters provide topographic information on other planets, particularly Venus. See also Automatic landing system; Ground proximity warning system.
Like other radar devices, the altimeter measures distance by determining the time required for a radio wave to travel to and from a target, in this case the Earth's surface. If the Earth were a perfectly flat horizontal plane or smooth sphere, the signal would come only from the closest point, and would be a true measure of altitude. Actually, the Earth is not smooth, and energy is scattered back to the radar from all parts of the surface illuminated by the transmitter. For the radar to measure distance to the ground accurately, it must distinguish between the energy from points near the vertical and that from more distant points.
Most radio altimeters use either pulse or frequency modulation, the former being more popular for high altitudes, and the latter for low altitudes. In a typical pulse altimeter the radio-frequency carrier is modulated with short pulses (under 0.25 microsecond). The short pulse permits measurements, even at low altitudes, of the time delay between the leading edge of the transmitted pulse and that of the pulse returned from the ground. Early pulse altimeters displayed the received signal on a cathode-ray tube with circular sweep, allowing the pilot to determine the leading-edge position of the echo signal. Modern pulse altimeters use a tracking gate system. One gate is kept close to the leading edge by a servo system that adjusts the position of the gate to the optimum delay point. A simple single-gate system can be used, but most pulse altimeters use two or three gates to achieve better distance measurement in the presence of noise and fading. See also Pulse modulator.
In a frequency-modulated (FM) altimeter, the frequency of a continuous carrier is swept in some manner, usually to give a triangular frequency-time curve. The difference in frequency between that received from the ground (but transmitted earlier) and that being transmitted is a measure of the time delay. See also Frequency modulation.