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Field Value Parameter<br />

x + 5 X<br />

x + 6 X-rate<br />

x + 7 Y<br />

x + 8 Y-rate<br />

x + 9 Z<br />

x + 10 Z-rate<br />

x + 11 Azimuth<br />

x + 12 Azimuth rate<br />

x + 13 Elevation<br />

x + 14 Elevation Rate<br />

x + 15 Rotation<br />

x + 16 Rotation Rate<br />

For these field values, x is the index of the particular articulated part shown below.<br />

Index Articulated Part<br />

1024 rudder<br />

1056 left flap<br />

1088 right flap<br />

1120 left aileron<br />

1152 right aileron<br />

1184 helicopter - main rotor<br />

1216 helicopter - tail rotor<br />

1248 other Aircraft Control Surfaces defined as needed<br />

2048 periscope<br />

2080 generic antenna<br />

2112 snorkel<br />

2144 other extendible parts defined as needed<br />

3072 l<strong>and</strong>ing gear<br />

3104 tail hook<br />

3136 speed brake<br />

3168 left weapon bay door<br />

3200 right weapon bay doors<br />

3232 tank or APC hatch<br />

3264 wingsweep<br />

3296 Bridge launcher<br />

3328 Bridge section 1<br />

3360 Bridge section 2<br />

3392 Bridge section 3<br />

3424 Primary blade 1<br />

3456 Primary blade 2<br />

3488 Primary boom<br />

457<br />

Section 4.7<br />

Parameter Type

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