Gillham Code - Altitude Encoder

Altitude Encoder

An altitude encoder takes the form of a small metal box containing a pressure sensor and signal conditioning electronics. The pressure sensor is often heated, which requires a warm-up time during which height information is either unavailable or inaccurate. Older style units can have a warm-up time of up to 10 minutes; more modern units warm up in less than 2 minutes. Some of the very latest encoders incorporate unheated 'instant on' type sensors. During the warm-up of older style units the height information may gradually increase until it settles at its final value. This is not normally a problem as the power would typically be applied before the aircraft enters the runway and so it would be transmitting correct height information soon after take-off.

A common configuration is for the transponder to supply power to the encoder only in the altitude reporting (mode C) setting. This could be problematic if mode C is selected in flight as the warm-up time would start from that point. Height information may not then be transmitted to the SSR station for up to 10 minutes. The purpose of the encoder supply switching via the transponder is to reduce power consumption. Typically an encoder will require about 5 W whilst the heater is engaged. The heater cycles on and off during operation and is controlled by the conditioning circuitry. The duty cycle varies according to the ambient temperature conditions.

Light aircraft electrical systems are typically 12 V or 28 V. To allow seamless integration with either, the encoder uses a number of open-collector (open-drain) transistors to interface to the transponder. The height information is represented as 11 binary digits in a parallel form using 11 separate lines designated D2 D4 A1 A2 A4 B1 B2 B4 C1 C2 C4. The Gillham code contains a D1 bit but this is unused in practical applications.

Different classes of altitude encoder do not use all of the available bits. All use the A, B and C bits; increasing altitude limits require more of the D bits. Up to and including 30700 ft does not require any of the D bits. This is suitable for most light general aviation aircraft. Up to and including 62700 ft requires D4. Up to and including 126700 ft requires D4 and D2. Note that D1 is never used.

The datum used by altitude encoders is −1200 ft although many will not output anything lower than −1000 ft. Negative flight levels are included in the code to permit altitude measurement at low levels when the ambient pressure is high.

Note that the altitude code output by a standard altitude encoder is a pressure altitude. That is to say, it is always with respect to a pressure datum of 1013.2 mBar (hectopascals) or 29.92 inHg. It does not indicate the height above sea level (altitude) or the ground (height). Pressure altitudes are referred to as flight levels and are expressed to the nearest 100 ft. For clarity here is a sample of the Gillham code from 0 ft to 1000 ft; note that 1000 ft is equivalent to a flight level of 10.

ALTITUDE D1 D2 D4 A1 A2 A4 B1 B2 B4 C1 C2 C4
0 0 0 0 0 0 0 0 1 1 0 1 0
100 0 0 0 0 0 0 0 1 1 1 1 0
200 0 0 0 0 0 0 0 1 1 1 0 0
300 0 0 0 0 0 0 0 1 0 1 0 0
400 0 0 0 0 0 0 0 1 0 1 1 0
500 0 0 0 0 0 0 0 1 0 0 1 0
600 0 0 0 0 0 0 0 1 0 0 1 1
700 0 0 0 0 0 0 0 1 0 0 0 1
800 0 0 0 0 0 0 1 1 0 0 0 1
900 0 0 0 0 0 0 1 1 0 0 1 1
1000 0 0 0 0 0 0 1 1 0 0 1 0

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