نتایج جستجو برای: inertial navigation system

تعداد نتایج: 2269767  

Accurate alignment and vertical channel instability play an important role in the strap-down inertial navigation system (SINS), especially in the case that precise navigation has to be achieved over long periods of time. Due to poor initialization as well as the cumulative errors of low-cost inertial measurement units (IMUs), initial alignment is not sufficient to achieve required navigation ac...

Journal: :international journal of electrical and electronics engineering 0
mahdi fathi department of aerospace engineering, malek ashtar university of technology nematollah ghahramani faculty/ department of electrical engineering, malek ashtar university of technology mohammad ali shahi ashtiani faculty/ department of aerospace engineering, malek ashtar university of technology mohsen fallah faculty/ department of electrical engineering, malek ashtar university of technology ali mohammadi faculty/department of aerospace engineering, malek ashtar university of technology

against the range-dependent accuracy of the tracking radar measurements including range, elevation and bearing angles, a new hybrid adaptive kalman filter is proposed to enhance the performance of the radar aided strapdown inertial navigation system (ins/radar). this filter involves the concept of residual-based adaptive estimation and adaptive fading kalman filter and tunes dynamically the fil...

Obviously navigation is one of the most complicated issues in mobile robots. Intelligent algorithms are often used for error handling in robot navigation. This Paper deals with the problem of Inertial Measurement Unit (IMU) error handling by using Extended Kalman Filter (EKF) as an Expert Algorithms. Our focus is put on the field of mobile robot navigation in the 2D environments. The main chall...

Obviously navigation is one of the most complicated issues in mobile robots. Intelligent algorithms are often used for error handling in robot navigation. This Paper deals with the problem of Inertial Measurement Unit (IMU) error handling by using Extended Kalman Filter (EKF) as an Expert Algorithms. Our focus is put on the field of mobile robot navigation in the 2D environments. The main chall...

Against the range-dependent accuracy of the tracking radar measurements including range, elevation and bearing angles, a new hybrid adaptive Kalman filter is proposed to enhance the performance of the radar aided strapdown inertial navigation system (INS/Radar). This filter involves the concept of residual-based adaptive estimation and adaptive fading Kalman filter and tunes dynamically the fil...

ژورنال: مهندسی دریا 2018

Time-growing navigation error due to inevitable measurement errors in the MEMS-grade inertial sensor is one of the main challenges in low-cost inertial navigation systems (INSs). This paper aims to develop AHRS/GPS/DR integrated navigation algorithm for long-range autonomous underwater vehicle (AUV). Proper performance in deals with long-term GPS outage is the main advantage of the proposed low...

پایان نامه :وزارت علوم، تحقیقات و فناوری - دانشگاه علم و صنعت ایران - دانشکده مهندسی برق 1387

ناوبری اینرسی یکی از روش های تعیین موقعیّت جسم متحرّک است که بر اساس قوانین نیوتن عمل می-کند. به دلایلی گوناگون، این سیستم در معرض خطای رشد کننده است و از این رو، تحلیل خطاها و نیز اصلاح آن به کمک ترکیب اطّلاعات با سیستم های کمک ناوبری مورد بررسی در بسیاری از مقالات قرار گرفته است. در این پایان نامه، ابتدا روش ناوبری اینرسی بررسی شده و معادلات حاکم که منجر به استخراج وضعیّت، سرعت و موقعیّت از داده ه...

Journal: :Electrical and data processing facilities and systems 2018

Dadi, Gh. Mohammad, Pariz, N.,

The estimation of situation in a combinational navigation GPS/INS with least number of satellites is the main purpose of this paper. As inertial measurement unit uses altimeter for height measurement, we can assume which height poses certain amounts, whereas geographical length and width are unknown to us in this paper. The single difference GPS is employed for updating the inertial navigation ...

پایان نامه :وزارت علوم، تحقیقات و فناوری - دانشگاه صنعتی خواجه نصیرالدین طوسی - دانشکده مهندسی برق 1381

خطای سیستم ناوبری اینرسی با گذشت زمان افزایش می یابد در نتیجه برای دستیابی به دقت بالاتر مخصوصا در ناوبری طولانی مدت نیاز به سیستم های کمکی است. سیستم تعیین موقعیت جهانی با توجه به خواص مکمل خود با سیستم ناوبری اینرسی مناسب ترین سیستم کمکی محسوب می شود. در این پروژه پس از شبیه سازی gps و ins خاص، تلفیق متوالی و کامل آنها مورد بررسی و شبیه سازی قرار می گیرد و سپس این دو روش تلفیق با هم مقایسه می...

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