Certus Reference Manual • Advanced Navigation Packet Protocol
10.5.5.1 Alignment DCM
The alignment DCM (Direction Cosine Matrix) is used to represent an alignment offset of Certus from its
standard alignment. A DCM is used rather than Euler angles for accuracy reasons. To convert Euler angles to
DCM, use the formula below with angles in radians.
DCM[0][0] = cos(heading) * cos(pitch)
DCM[0][1] = sin(heading) * cos(pitch)
DCM[0][2] = -sin(pitch)
DCM[1][0] = -sin(heading) * cos(roll) + cos(heading) * sin(pitch) * sin(roll)
DCM[1][1] = cos(heading) * cos(roll) + sin(heading) * sin(pitch) * sin(roll)
DCM[1][2] = cos(pitch) * sin(roll)
DCM[2][0] = sin(heading) * sin(roll) + cos(heading) * sin(pitch) * cos(roll)
DCM[2][1] = -cos(heading) * sin(roll) + sin(heading) * sin(pitch) * cos(roll)
DCM[2][2] = cos(pitch) * cos(roll)
10.5.6 Filter Options Packet
Filter Options Packet
Packet ID
Length
Read / Write
Field #
Bytes Offset
1
0
2
1
3
2
4
3
5
4
6
5
7
6
8
7
9
8
10
9
11
10
Table 138: Filter Options Packet
10.5.6.1 Vehicle Types
Value
0
1
2
v2.4
Data Type
Size
u8
1
u8
1
u8
1
u8
1
u8
1
u8
1
u8
1
u8
1
u8
1
u8
1
7
Description
Unlimited
Bicycle or Motorcycle
Car
186
17
Read / Write
Description
Permanent
10.5.6.1 Vehicle Types
Internal GNSS enabled (boolean)
Magnetic Heading enabled (boolean)
Atmospheric altitude enabled (boolean)
Velocity heading enabled (boolean)
Reversing detection enabled (boolean)
Motion analysis enabled (boolean)
Automatic magnetic calibration enabled (boolean)
Dual antenna disabled
Reserved (set to zero)
Page 191
2024-12-17
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