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)
13.10.5
Filter Options Packet
Packet ID
Length
Field
Bytes
#
Offset
1
0
2
1
3
2
4
3
5
4
6
5
7
6
8
7
9
8
Table 101: Filter options packet
Filter Options Packet
Data
Size
Type
u8
1
u8
1
u8
1
u8
1
u8
1
u8
1
u8
1
u8
1
u8
9
Spatial FOG Dual Reference Manual
Description
Permanent
Vehicle type, see section 13.10.5.1
Internal GNSS enabled (boolean)
Reserved (set to zero)
Atmospheric altitude enabled (boolean)
Velocity heading enabled (boolean)
Reversing detection enabled (boolean)
Motion analysis enabled (boolean)
Reserved (set to zero)
Page 128 of 138
Version 1.0
26/06/2015
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