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GPS Implementation by Peter Muehlenbrock ("Salvo") for Mikrokopter/FlightCrtl
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GPS Implementation by Peter Muehlenbrock ("Salvo") for Mikrokopter/FlightCrtl
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As of Jan, 9th 2007
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As of Jan, 20th 2007
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Please note the files Licensce_LPGL.txt and Licensce_GPL.txt
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Please note the files Licensce_LPGL.txt and Licensce_GPL.txt
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This SW is based on Holgers V00.67g.
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This SW is based on Holgers V00.67g.
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Hardware-requirements: 
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Hardware-requirements: 
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Calibrated compass of type CMPS03, horizontally adjusted
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Calibrated compass of type CMPS03, horizontally adjusted
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Please calibrate the ACC Sensor values (pitch full, yaw full right) in horizontal orientation of the kopter 
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Please calibrate the ACC Sensor values (pitch full, yaw full right) in horizontal orientation of the kopter 
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as exactly as possible.
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as exactly as possible.
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Parameters:
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Parameters:
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The GPS Hold regulator is of type PID: UserParameter1 =P(proportional), UserParameter2 = I(ntegral), 
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The GPS Hold regulator is of type PID: UserParameter1 =P(proportional), UserParameter2 = I(ntegral), 
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UserParameter3 = D(ifferential). Standardvalues for P,I and D are 80,0,120.
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UserParameter3 = D(ifferential). Standardvalues for P,I and D are 80,16,80.
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The i-Part may be set to 0 if a small deviation from hold position is acceptable. The D-Part is important to avoid 
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The I-Part may be set to 0 if a small deviation from hold position is acceptable. The D-Part is important to avoid 
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oscillating. 
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oscillating. 
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Please find out the best values yourself. 
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Please find out the best values yourself. 
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It might be useful to put the P and D Part on potis and test the behaviour in flight.
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It might be useful to put the P and D Part on potis and test the behaviour in flight.