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Stochastic modeling of inertial sensor errors for loosely coupled INS /GPS integrated navigation system / Abdalla Suliman Elhadi Kraza ; Supervised Sayed Desouki Hasan , Gamal Mahmoud Elbayoumi , Mohamed Sayed Bayoumi

By: Contributor(s): Material type: TextTextLanguage: English Publication details: Cairo : Abdalla Suliman Elhadi Kraza , 2011Description: 204 P. : charts , facsimiles ; 30cmOther title:
  • النمذجة العشوائية لاخطاء مجسمات القصور الذاتى لنظام ملاحى متكامل باستخدام الاقمار الصناعية لانظمة القصور الذاتى [Added title page title]
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  • Issued also as CD
Dissertation note: Thesis (Ph.D.) - Cairo University - Faculty of Engineering - Department of Aerospace Engineering Summary: The aim of the thesis is to build and raise the efficiency of navigation system for air vehicles by using integrated navigation system which consists of Inertial Navigation System (INS) and Global Position System (GPS) .To raise the efficiency of the integrated navigation system it is necessary to model the stochastic sensor errors to be augmented in the strap down INS error model so that an integrated navigation system built using extended kalman filter
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Item type Current library Home library Call number Copy number Status Date due Barcode
Thesis Thesis قاعة الرسائل الجامعية - الدور الاول المكتبة المركزبة الجديدة - جامعة القاهرة Cai01.13.01.Ph.D.2011.Ab.S (Browse shelf(Opens below)) Not for loan 01010110056379000
CD - Rom CD - Rom مخـــزن الرســائل الجـــامعية - البدروم المكتبة المركزبة الجديدة - جامعة القاهرة Cai01.13.01.Ph.D.2011.Ab.S (Browse shelf(Opens below)) 56379.CD Not for loan 01020110056379000

Thesis (Ph.D.) - Cairo University - Faculty of Engineering - Department of Aerospace Engineering

The aim of the thesis is to build and raise the efficiency of navigation system for air vehicles by using integrated navigation system which consists of Inertial Navigation System (INS) and Global Position System (GPS) .To raise the efficiency of the integrated navigation system it is necessary to model the stochastic sensor errors to be augmented in the strap down INS error model so that an integrated navigation system built using extended kalman filter

Issued also as CD

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