INTEGRATED INERTIAL NAVIGATION WITH POSITIONING SYSTEM FOR INCREASING ORBITAL MODULE NAVIGATION ACCURACY

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JAFARI MAHDI; SANGARY ARASH; ROSHANIAN JAFAR

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Journal Paper

Paper Information

Journal: Journal of Space Science and Technology Year:2012 | Volume:5 | Issue:3 (12) Page(s): 11-19

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Information Journal Paper

Title

INTEGRATED INERTIAL NAVIGATION WITH POSITIONING SYSTEM FOR INCREASING ORBITAL MODULE NAVIGATION ACCURACY

Author(s)

JAFARI MAHDI | SANGARY ARASH | ROSHANIAN JAFAR | Issue Writer Certificate

Keywords

INTEGRATED NAVIGATIONQ2

KALMAN FILTERQ2

INERTIAL NAVIGATIONQ2

POSITIONING SYSTEMQ1

Abstract

The INERTIAL NAVIGATION system is an ideal solution for motion detection with high accuracy with fast dynamics, but the precise location and status of the system output can be significantly reduced over time. On the other hand, global POSITIONING SYSTEM is able to determine its position with an average accuracy around the earth. But the GPS alone isn’t enough for navigation of orbital modules, because it doesn’t have situation of orbital modules. The integrated INERTIAL NAVIGATION system with global POSITIONING SYSTEM is a low cost method of providing an accurate and reliable navigation system in the civilian and military aerospace applications. In this paper, using the extended KALMAN FILTER, we design an algorithm to estimate error of sensors, navigation and GPS. This method can be widely used in the INTEGRATED NAVIGATION INS / GPS in aerospace applications and provides an accurate navigation.

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APA: Copy

JAFARI, MAHDI, SANGARY, ARASH, & ROSHANIAN, JAFAR. (2012). INTEGRATED INERTIAL NAVIGATION WITH POSITIONING SYSTEM FOR INCREASING ORBITAL MODULE NAVIGATION ACCURACY. JOURNAL OF SPACE SCIENCE AND TECHNOLOGY (JSST), 5(3 (12)), 11-19. SID. https://sid.ir/paper/149957/en

Vancouver: Copy

JAFARI MAHDI, SANGARY ARASH, ROSHANIAN JAFAR. INTEGRATED INERTIAL NAVIGATION WITH POSITIONING SYSTEM FOR INCREASING ORBITAL MODULE NAVIGATION ACCURACY. JOURNAL OF SPACE SCIENCE AND TECHNOLOGY (JSST)[Internet]. 2012;5(3 (12)):11-19. Available from: https://sid.ir/paper/149957/en

IEEE: Copy

MAHDI JAFARI, ARASH SANGARY, and JAFAR ROSHANIAN, “INTEGRATED INERTIAL NAVIGATION WITH POSITIONING SYSTEM FOR INCREASING ORBITAL MODULE NAVIGATION ACCURACY,” JOURNAL OF SPACE SCIENCE AND TECHNOLOGY (JSST), vol. 5, no. 3 (12), pp. 11–19, 2012, [Online]. Available: https://sid.ir/paper/149957/en

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