Spatial FOG Reference Manual
Page 133 of 144
Version 2.3
03/05/2018
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
Filter Options Packet
Packet ID
186
Length
17
Field
#
Bytes
Ofset
Data
Type
Size
Description
1
0
u8
1
Permanent
2
1
u8
1
Vehicle type, see section 13.10.5.1
3
2
u8
1
Internal GNSS enabled (boolean)
4
3
u8
1
Reserved (set to zero)
5
4
u8
1
Atmospheric altitude enabled (boolean)
6
5
u8
1
Velocity heading enabled (boolean)
7
6
u8
1
Reversing detection enabled (boolean)
8
7
u8
1
Motion analysis enabled (boolean)
9
8
u8
9
Reserved (set to zero)
Table 100: Filter options packet