by eanrsmoAim Cfg Cs 100 Hsl
Aim Cfg Cs 100 Hsl
the command position is normally set to 0, but can be set to the following positions:
- 0: do not link
- 1: link using an encrypted packet
- 2: link using the synchronous telemetry link
- 3: link using the semi-synchronous telemetry link
- 4: link using the asynchronous telemetry link
the cell system is a low-power cellular network that allows pilots to exchange messages with ground stations. the system is capable of establishing two-way communication while the aircraft is at cruise speeds up to approximately 380 knots. this is a safety feature, as it allows ground stations to contact an aircraft if it strays off course and subsequently makes a distress call.
the time between establishing a link is controlled by the acc link switch, also on the iff antenna control/test panel panel. the switch settings should be based on your position, flying conditions and desired link time of 1.5 minutes to establish a link between the two aircraft.
the avb-link switch provides the link between the two f-14’s avionics systems, it is used to receive emergency messages between the aircraft and if the f-14 has been damaged or the cockpit in some other way entered an otherwise unrecoverable state. this was formerly known as the joint link, before being replaced by the avb-link switch.
the controls on the ddd stick are: the action trigger switch (5), elevation vernier control (4), the offset button (3) and the mrl button (2). the action trigger on the left side of the stick has two detents, the half-action first detent and the full-action second detent. half-action enables display of the cursor for the selected mode except when in ddd cursor mode where it enables stick control of ddd elevation and azimuth. in the tid mode it additionally enables the super fast search mode in the tid (see chapter about radar transitional modes for more information). full-action, when enabled tells the tid to lockon to a target in the tid mode if a target is present in its acquisition gates. in the ddd mode it marks the current cursor position if present or, if not present, sets the ddd cursor to the pre-bootup home position. the offset button on the right side of the stick, when enabled, moves the own aircraft symbol from the dock ifd to the position indicated by the tid (or gps if that is selected) or ddd cursor.
you can enable the movement of the hcu via the move stick button. the move stick button has a timer on it which has a maximum of 30 seconds to turn on, off or reset. the timer has been implemented to prevent accidental movement of the stick when the aircraft is not in x mode (autopilot off) and therefore more time is required to move the hcu to control the tid cursor.
the two control elements just to the right of the elevation vernier control are the elevation quarter-points. in the radar mode the range and rate verniers are set to the relevant half-circles on the other two axis and the tcs mode rotates them clockwise so that the fourth quarter-circle is centered on the cursor. moving this quarter-circle with the rotary encoder and the elevation vernier controls will change the lock-on range and rate and the deflection of the cursor. the sixth and ninth quarter-circles are the slider controls for changing the elevation angle control loops, around the rising edge of the elevation lobe (se, or normal). in the radar mode the first slider controls the antenna tilt relative to the azimuth rotation, for example when steering north the radar will tilt away from the aircraft heading as the radars would point towards north when tracking north american p-51 mustangs. the second slider controls the steepness of the elevation lobe. higher values change the shape of the elevation lobe from an undistorted half-circle to a straight line. as a result only the first quarter-circle is visible at the maximum tilt. lower values invert the shape back to a half-circle. in the radar mode the third and fourth quarter-circles are the rate verniers for the range and rate range loops. in the radar mode the range loop is moved along the horizontal axis from left to right and the rate loop rotated through the vertical axis from bottom to top. when both rotational and translational axes are moving they operate independently. in the radar mode the last and least visible quarter-circle is the scan button, it tells the radar to “spin” the antenna baseplate for the current lobe. the slider controls will not move in the radar mode. in all other modes the last quarter-circle is the ddd sweep button. it tells the radar to first lock on to the first acquisition gate in the ddd mode, switch to the second acquisition gate in the tid mode, and then try to lock on to the last acquisition gate in the tcs mode, simulating a 3d sweep from the nose to the tail of the aircraft (the only exception being the 10/40 mode in which the radar is always locked onto the last acquisition gate until the mission is completed.) the ddd and tid modes are used for while-scan acquisition, the tcs mode is used for real time tracking when only single gate ddd and tid modes can be used, and the 10/40 mode is used if (and only if) double gate ddd and tid acquisition modes are not available.
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