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Avionics / Navigation / Missile guidance / Inertial navigation system / GPS/INS / Global Positioning System / Inertial measurement unit / Gyroscope / Kalman filter / Technology / Aerospace engineering / Aircraft instruments


An Integrated Low Cost GPS/INS Attitude Determination and Position Location System Robert Wolf, Guenter W. Hein, Bernd Eissfeller, Erwin Loehnert Institute of Geodesy and Navigation (IfEN), University FAF Munich, D-85577
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Document Date: 2010-06-30 09:18:59


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File Size: 140,50 KB

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City

Munich / Wiley-Interscience / London / /

Company

Data / Inertial Navigation Software / Vice / MotionPak Computer / Intel / Trimble Navigation Ltd / GPS Laboratory / /

Currency

USD / /

Facility

University FAF Munich / Munich University of Technology / Base station / Erwin Loehnert Institute of Geodesy / Institute of Geodesy / GPS Laboratory / University of Federal Armed Forces Munich / University FAF Schmidt / /

IndustryTerm

navigation systems / real time processing / aerospace engineering / In real time mode / filter software / strapdown algorithms / attitude solutions / navigation software / post processing / post mission processing / real time processing capability / satellite geodesy / differential carrier phase measurements / realtime navigation software / /

Organization

Institute of Geodesy and Navigation / University of Federal Armed Forces Munich / Erwin Loehnert Institute of Geodesy and Navigation / US Federal Reserve / Munich University of Technology / /

Person

Robert Wolf / Erwin Loehnert / Guenter W. Hein / Bernd Eissfeller / Sydney Toronto Eissfeller / /

Position

author / Professor and Director / Head / Research Associate / /

Product

Kalman / Trimble Advanced Navigation Sensor / /

ProgrammingLanguage

C / /

ProvinceOrState

New York / /

Technology

GPS system / Laser / technology of low cost solid-state inertial sensors / GPS / 486 processor / strapdown algorithms / /

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