GNSS BASED RELATIVE NAVIGATION FOR INTENTIONAL APPROXIMATION OF AIRCRAFT

Author:

Schielin Emmanuel1,Dautermann Thomas2

Affiliation:

1. SAGEM, Inertial Measurement Unit R&D Department

2. German Aerospace Centre (DLR), Institute of Flight Guidance

Abstract

In aviation, satellite navigation is generally only used to determine the absolute position of aircraft. We show that the signals can also be used for safe relative navigation provided that a data link exists between the two aircraft. The link can be used to form a double difference combination of code phase measurements and determine a three dimensional baseline vector. The baseline vector is protected by protection levels which determine the 3×10−7 error bound of the baseline estimation. Thus, the distance vector can be used to perform safe approximation maneuvers in instrument weather conditions. We derive the protection level expression and test the baseline vector estimation using data from two real satellite navigation receivers on the ground. Moreover, we simulate an intercept mission using a Spirent GNSS7790 simulator and show that with the derived protection bounds an approximation up to 10 m is possible.

Publisher

Vilnius Gediminas Technical University

Subject

Aerospace Engineering

Reference4 articles.

1. Cosentino, R. J.; Diggle, D. W.; De Haag, M. U.et al. 2006.Understanding GPS: Principles and Applications. Artech House, 379–458.

2. Short distance GPS models

3. Leva, J.; De Haag, M. U.; Van Dyke, K. 2006.Understanding GPS: Principles and Applications. Artech House, 301–375.

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