5 tracking problems – Research Concepts RC2000C User Manual

Page 47

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RC2000C Az/El Tracking Antenna Controller

Chapter 4

Inclined Orbit Satellites

39

Research Concepts, Inc. • 5420 Martindale Road • Shawnee, Kansas • 66218-9680 • USA

www.researchconcepts.com

Please review the description of TRACK mode in chapter 5 for a complete explanation of each of the

TRACK mode submodes and the TRACK mode menu system. Every field of every display screen is

described in that section.

4.4.5 Tracking Problems

This section discusses problems that can occur while tracking an inclined orbit satellite. TRACK mode

contains an ERROR submode, which displays an error message when it is active. Chapter 7 discusses

all of the possible errors that can occur. This section discusses the more common problems.

The LIMIT error occurs when an antenna limit (either azimuth or elevation) is encountered when

tracking an inclined orbit satellite. This error will only occur while the STEP TRACK or PROGRAM

TRACK submodes are active. The SEARCH submode will not attempt to move outside of the azimuth

or elevation limits. This error generally means that the azimuth or elevation (usually elevation) limits are

not set wide enough.

A PEAK LIMIT error indicates that the controller had to move the antenna too far during a STEP TRACK

peaking operation. The maximum movement of the antenna from the starting position for a STEP

TRACK operation is limited. This is to prevent the antenna from peaking up on an adjacent satellite.

This problem can be caused by a number of situations:

1. Specifying too large of an antenna diameter, or specifying Ku band when tracking a C band

satellite. These cause the controller to calculate too narrow of an antenna beamwidth. This

beamwidth is used to determine the maximum allowable movement from the starting position for a

STEP TRACK operation.

2. Specifying too small of a satellite inclination. In STEP TRACK mode, the controller performs

peakups often enough to avoid exceeding the maximum antenna pointing error specified by the

Max Track Error CONFIG mode item. If the specified satellite inclination is too small, the peakups

will not occur often enough, and the antenna may move far enough during a peakup to trigger the

PEAK LIMIT error.

3. The C Band AGC Threshold or the K/L Band AGC Threshold is set too low. If the threshold values

are set too low, when the transponder powers down, the AGC signal of the receiver may be above

the threshold when the antenna is looking at noise. In this case the controller would mistakenly

assume that the satellite signal is present, and attempt to peak up on the noise.

4. If the error occurs during a peakup operation while the PROGRAM TRACK sub-mode is active, it

may be that the Update Check Interval TRACK mode MENU item is set too large.

5. There may not be a sufficient number of position counts per degree of antenna movement about

one of the antenna axis. The controller cannot move less than one count. If a move of less than

one count is specified the antenna will round the step size up to one count. Note that all systems

will have one count of play or looseness in the antenna - see the next section. A good rule of thumb

is that there should be 10 position counts over the antenna’s 3-dB beamwidth for each axis.

6. Play or looseness in the mount can cause many problems. The user can test for play by shaking

the antenna. Another test is to see if the antenna peaks on a satellite at different count values

depending on which way the antenna approached the satellite. Here's an example. In one case

the peak is approached by jogging the antenna up and the peak occurs at 110 counts. In another

case the peak is approached by jogging the antenna down and the peak occurs at 103 counts. This

indicates that there are 7 counts of play in the system. The solution is to get rid of the play. In

some cases, increasing the Max Track Error parameter can help. In general, however, the

controller is not very tolerant of looseness in the mount.

If a linear actuator is used to drive the antenna about an axis, it usually forms one side of a triangle. As

the length of the linear actuator changes, the opposite angle varies and the pointing angle of the

antenna is changed. If the linear actuator has some play in it, the change in the antenna pointing angle

due to the play in the actuator can be minimized if the other sides of the triangle are made longer. In

some cases, the ball pivot often found on one side of the linear actuator is also loose. Anything which

can be done to tighten up the ball pivot will help.

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