Skip to main content
Log in

Precision aircraft attitude determination with multi-antennae GPS receivers

  • Published:
Gyroscopy and Navigation Aims and scope Submit manuscript

Abstract

Attitude determination is a central problem to aircraft navigation for a wide variety of applications, i.e. airborne laser scanning, airborne gravimetry etc. Standard multi-antennae attitude determination, relying on typically four antennae, provides an attitude accuracy of about 0.1°–0.3° per epoch, where usual update rates are of the order of 5–10 /s; while the noise is quite big, the stability with time is excellent. However, phase centre, multi path and antennae near field effects may cause significant biases or slowly varying effects. On the other hand, gyros may provide attitude information at very high sampling rates and at significantly higher resolutions, however, most are prone to significant drift effects, except e.g., laser gyros of highest precision. For an optimal configuration in economical, operational and accuracy aspects, it is worth to invest also in an advanced multi-antennae GNSS receiver. On these grounds, we acquired a GNATTI antennae receiver of Geo++ company, assembled of typically eight single L1-receivers. The redundancy of this set allows to do an antenna calibration for antennae phase centre, near field, and multipath effects. We did a number of tests both at a test stand and also with an aircraft with various receivers. The paper discusses some details and test results.

This is a preview of subscription content, log in via an institution to check access.

Access this article

Price excludes VAT (USA)
Tax calculation will be finalised during checkout.

Instant access to the full article PDF.

Similar content being viewed by others

Abbreviations

ADC:

Analog-to-Digital-Converter

CTS:

Conventional Terrestrial Reference System

FRD:

Forward, Right, Down (for body reference frame)

GNSS:

Global Navigation Satellite System such as GLONASS

GPS:

Global Positioning system

MA:

Multi-Antennae

SAGS4:

Strapdown Airborne Gravimetry System, prototype no. 4

References

  1. Arbinger, C., Enderle, W., Fraiture, L., and Wagner, O., A New Algorithm (Star) for Sycle Ambiguity Resolution within GPS Based Attitude Determination, 1999.

  2. Boedecker, G., Sensor Orientation from Multi-Antennae GPS and Gyros, Vortrag, Proceedings, 12th Saint Petersburg International Conference on Integrated Navigation Systems, 2005, pp. 17–24.

  3. Boedecker, G. and Stürze, A., SAGS4—StrapDown Airborne Gravimetry System Analysis, in Observation of the Earth System from Space, Flury, J., Rummel, R., Reigber, C., Rothacher, M., Boedecker, G., and Schreiber, U., Eds., Heidelberg: Springer, 2006, pp. 463–478.

    Chapter  Google Scholar 

  4. Brzezinska, D.A., Direct Sensor Orientation in Airborne and Land-Based Mapping Applications, Geod. Geoinf. Sci., The Ohio State University, Report no. 461, 2001.

  5. Enderle, W., Lagebestimmung von Satelliten in hochexzentrischen Orbits, basierend auf GPS Messungen, Ph.D.-Thesis, TU Berlin, 1998.

  6. Jekeli, C., Inertial Navigation Systems with Geodetic Applications, de Gruyter, 2001.

  7. Schade, H., Neigungsbestimmung mit GPS für die Photogrammetrie, Univ. Stuttgart, Dep. Geodesy and Geoinformatics, Rep. 2002.

  8. Schleppe, J.B., Interface and Performance Evaluation of u-blox LEA-4T (Antaris4 Chipset) for Attitude Determination Using HEADRT+, PLAN, Geomatics, UCalgary, 2006.

  9. Schleppe, J.B., Development of a Real-Time Attitude System Using a Quaternion Parametrization and a Non-Dedicated GPS Receiver, Univ. Calgary, Geomatics, UCGE Rep. no. 20096, 1996.

  10. Schmitz, M., Special Tests of Phase Center Variations of Various GPS Antennas and Some Results, Schmitz, M., Ed. [Spezielle Untersuchungen und Ergebnisse zum PCV von GPS-Antennen, Wissenschaftliche Arbeiten Fachrichtung Vermessungswesen an der Universität Hannover, Festschrift Prof. G. Seeber zum 60, Geburtstag, Nr. 239, Hannover, 2001, pp. 101–112.

  11. Schmitz, M., Wübbena, G., and Boettcher, G., Near Field Effects of a Car Roof on TPSHIPER-PLUS Phase Variations, Geo++®, Garbsen, White Paper, 2004.

  12. Wang, C., Development of a Low-cost GPS-Based Attitude Determination System, Univ.Calgary, Geomatics, UCGE, Rep. no. 20175, 2003.

  13. Wang, C. and Lachapelle, G., Development of a Low-Cost Solution for GPS/Gyro Attitude Determination, Proceedings of NTM, Conference, ION, 2004.

Download references

Author information

Authors and Affiliations

Authors

Additional information

Published in Russian in Giroskopiya i Navigatsiya, 2008, No. 4, pp. 21–29.

Rights and permissions

Reprints and permissions

About this article

Cite this article

Boedecker, G. Precision aircraft attitude determination with multi-antennae GPS receivers. Gyroscopy Navig. 1, 285–290 (2010). https://doi.org/10.1134/S2075108710040085

Download citation

  • Received:

  • Published:

  • Issue Date:

  • DOI: https://doi.org/10.1134/S2075108710040085

Keywords

Navigation