Zusammenfassung
Attitude estimation is the process of determining the spatial orientation of an object. A system formed by multiple Global Navigation Satellite System (GlossaryTerm
GNSS
) antennas placed at known relative positions acts as an attitude sensor. This chapter provides an overview of practical applications of GNSS-based attitude determination, gives the principles of attitude representation and estimation, and reviews a constrained ambiguity resolution method to reliably fix the carrier-phase integer ambiguities and obtain precise attitude estimations.Access this chapter
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Abbreviations
- DD:
-
double-difference
- ECEF:
-
Earth-centered Earth-fixed
- GNSS:
-
global navigation satellite system
- GPS:
-
Global Positioning System
- ILS:
-
integer least-squares
- IMU:
-
inertial measurement unit
- INS:
-
inertial navigation system
- ISS:
-
International Space Station
- LAMBDA:
-
least-squares ambiguity decorrelation adjustment
- LEO:
-
low Earth orbit
- MEMS:
-
micro-electromechanical system
- NASA:
-
National Aeronautics and Space Administration
- PMF:
-
probability mass function
- RMS:
-
root mean square
- SD:
-
single-difference
- UAV:
-
unmanned aerial vehicle
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Giorgi, G. (2017). Attitude Determination. In: Teunissen, P.J., Montenbruck, O. (eds) Springer Handbook of Global Navigation Satellite Systems. Springer Handbooks. Springer, Cham. https://doi.org/10.1007/978-3-319-42928-1_27
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