EasyManuals Logo

Inertial Labs INS-P User Manual

Inertial Labs INS-P
251 pages
To Next Page IconTo Next Page
To Next Page IconTo Next Page
To Previous Page IconTo Previous Page
To Previous Page IconTo Previous Page
Page #215 background imageLoading...
Page #215 background image
INS
GUI User’s Manual
Inertial Labs, Inc
TM
Address: 39959 Catoctin Ridge Street, Paeonian Springs, VA 20129 U.S.A.
Tel: +1 (703) 880-4222, Fax: +1 (703) 935-8377 Website: www.inertiallabs.com
215
0x5F
0x60
Odometer
4
integer
Odometer distance, m*1000
0x61
Air speed
2
sword
Air speed, kt*100
0x62
Wind data
8
sword
North wind, kt*100
sword
East wind, kt*100
word
North wind STD, kt*100
word
East wind STD, kt*100
0x63
External position
20
integer
Latitude external, deg*1.0e7
integer
Longitude external, deg*1.0e7
integer
Altitude external, m*1000
word
Latitude external STD, m*100
word
Longitude external STD, m*100
word
Altitude external STD, m*100
word
External position latency, sec*1000
0x64
Doppler shift
from locator
16
integer
Locator latitude, deg*1.0e7
integer
Locator longitude, deg*1.0e7
integer
Locator altitude, deg*1.0e7
sword
Doppler shift, m/s*100
word
Doppler shift STD, m/s*100
0x65
New aiding data
2
word
Indicator of update of external sensors
data (see Table C.12)
0x66
Heading external
6
word
Heading external, deg*100
word
Heading external STD, deg*100
word
Heading external latency, sec*1000
0x67
0x6F
Reserved
TBD
TBD
Notes:
1. Unit status word (USW) is highly recommended for choice to control INS unit state
(see Appendix D for details).
2. If even one data type from “GNSS data” group is chosen, then “New_GPS” data is
highly recommended for choice too. This is indicator of new update of GNSS data (see
Table C.6 for details).
3. If even one data type from “External aiding data” group is chosen, then “New aiding
data” is highly recommended for choice too. This is indicator of new update of aiding data
(see Table C.12 for details).
4. "UTC Decimal Seconds" are milliseconds part of the UTC time.
5. Values of KG, KA are scale factors depending on gyro and accelerometer range:
Gyro range, deg/sec
250 or 300
450 or 500
1000
2000
KG
100
50
20
10
Accelerometer range, g
2
4
6
8
10
15
40
KA
10000
8000
5000
4000
2000
2000
500
6. g = 9.8106 m/s
2
.

Table of Contents

Questions and Answers:

Question and Answer IconNeed help?

Do you have a question about the Inertial Labs INS-P and is the answer not in the manual?

Inertial Labs INS-P Specifications

General IconGeneral
BrandInertial Labs
ModelINS-P
CategoryCar Navigation system
LanguageEnglish