This paper, written at Safran Electronics & Defense as part of the author’s Master Thesis, is dedicated to the implementation of a GNSS alternate trajectory simulator for an aircraft GPS-aided Inertial Navigation System. First, the basic tenets of GPS-aided inertial navigation systems will be briefly reminded. The need for a GPS spoofing simulator will then be explained. The simulator architecture will be detailed, before showing the in-depth software implementation. Finally, the simulator performance will be ascertained to verify compliance with requirements.
| Identifer | oai:union.ndltd.org:UPSALLA1/oai:DiVA.org:kth-309599 |
| Date | January 2021 |
| Creators | Nguyen, Julien |
| Publisher | KTH, Flygdynamik |
| Source Sets | DiVA Archive at Upsalla University |
| Language | English |
| Detected Language | English |
| Type | Student thesis, info:eu-repo/semantics/bachelorThesis, text |
| Format | application/pdf |
| Rights | info:eu-repo/semantics/openAccess |
| Relation | TRITA-SCI-GRU ; 2021:377 |
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