Closed form position of airborne targets in new design of geometric constrained problem by bearing measurements

Article Type:
Research/Original Article (دارای رتبه معتبر)
Abstract:
Positioning involves a wide range of military and industrial applications. In a positioning based on directional measurement, the transmitter's position is the intersection of the hypothetical orientation lines that send out the sensors to the transmitter. In the absence of noise, the location of these lines will be unique. But in reality, existing noise causes uncertainty in measurements and positioning. So far, various approaches have been introduced for orientation measurement based positioning. Most of these methods are based on numerical algorithms and the traditional maximum likelihood in order to estimate the optimal target position. These methods are equivalent to minimizing the total measurement errors by assuming Gaussian noise. Although TML is accurate, but due to the use of a recursive numerical algorithm, when the noise measurements are large or the geometry of the problem is undesirable, it causes a divergence of algorithm. Because of the use of numerical algorithms, these methods do not have a mathematical closed form for the answer. In addition to these methods, limited efforts are made to solve the problem and extract the closed form answer based on the geometric properties of the problem, most notably the Stansfield method. This algorithm is based on the assumption that the Gaussian noise is small and that the transmitter's approximate distance from the sensors is known. In this paper, attention is paid to the geometric properties of the problem in order to extract the closed form answer. But the assumption of the small Gaussian noise and the approximate distance between the transmitter and the sensors are not required. In most papers, the response of the TML algorithm as a benchmark has been compared in order to determine the precision of the proposed method. In this paper, it is shown in several scenarios that the proposed algorithm has a lower RMSE error than the TML, in addition to providing a mathematical closed form answer.
Language:
Persian
Published:
Aerospace Science and Technology Journal, Volume:7 Issue: 1, 2018
Pages:
63 to 71
magiran.com/p1865018  
دانلود و مطالعه متن این مقاله با یکی از روشهای زیر امکان پذیر است:
اشتراک شخصی
با عضویت و پرداخت آنلاین حق اشتراک یک‌ساله به مبلغ 1,390,000ريال می‌توانید 70 عنوان مطلب دانلود کنید!
اشتراک سازمانی
به کتابخانه دانشگاه یا محل کار خود پیشنهاد کنید تا اشتراک سازمانی این پایگاه را برای دسترسی نامحدود همه کاربران به متن مطالب تهیه نمایند!
توجه!
  • حق عضویت دریافتی صرف حمایت از نشریات عضو و نگهداری، تکمیل و توسعه مگیران می‌شود.
  • پرداخت حق اشتراک و دانلود مقالات اجازه بازنشر آن در سایر رسانه‌های چاپی و دیجیتال را به کاربر نمی‌دهد.
دسترسی سراسری کاربران دانشگاه پیام نور!
اعضای هیئت علمی و دانشجویان دانشگاه پیام نور در سراسر کشور، در صورت ثبت نام با ایمیل دانشگاهی، تا پایان فروردین ماه 1403 به مقالات سایت دسترسی خواهند داشت!
In order to view content subscription is required

Personal subscription
Subscribe magiran.com for 70 € euros via PayPal and download 70 articles during a year.
Organization subscription
Please contact us to subscribe your university or library for unlimited access!