ACCURACY CHARACTERISTICS ESTIMATION OF SNS DIFFERENTIAL MODE USED TO GET AIRCRAFT TRAJECTORY PARAMETERS DURING FLIGHT TESTS

机译：飞行测试过程中用于获取飞机弹道参数的SNS差分模式的精度特征估计

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To obtain airplane trajectory parameters at flight tests realization implements differential operational mode usage of satellite navigational system instrumentation (SNS). The navigating parameters accuracy of a differential mode depends on the type of SNS receivers and data formation algorithms of the differential mode. The estimation of navigating parameters accuracy on various flight sites is a difficult task. In the work is carried out the data error estimation of SNS differential mode by various methods.

机译：为了在飞行测试中获得飞机的轨迹参数，实现实现了卫星导航系统仪器（SNS）的差分操作模式用法。差分模式的导航参数精度取决于SNS接收器的类型和差分模式的数据形成算法。估计各种飞行站点上的导航参数准确性是一项艰巨的任务。在工作中通过各种方法进行了SNS差模的数据误差估计。

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来源
《Saint Petersburg International Conference on Integrated Navigation Systems; 20050523-25; Saint Petersburg(RU)》|2005年|P.195-197|共3页
会议地点 Saint Petersburg(RU)
作者
Kopylov I.; Kharin E.; Polikarpov V.; Kopelovich V.;
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作者单位

FSUE 'Gromov Flight research institute' Zhukovsky, Russia;

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会议组织
原文格式 PDF
正文语种 eng
中图分类导航设备;
关键词
flight tests; trajectory measurements; a satellite navigating system receiver; an accuracy estimation of navigating parameters measurements;

机译：飞行测试;轨迹测量;卫星导航系统接收器;导航参数测量的准确性估计;

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1. Flight-Test Estimation of Aircraft Aerodynamic Characteristics-Russian Experience [J] . Yu. I. Sneshko, V. N. Chetvergov, T. A. Chernysheva Journal of Aircraft . 2005,第1期

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2. Parameter Estimation from Flight Data of Hansa-3 Aircraft Using Quasi-Steady Stall Modeling [J] . Rakesh Kumar, A. K. Ghosh, Ajay Misra Journal of aerospace engineering . 2013,第3期

机译：基于准稳态失速模型的Hansa-3飞机飞行数据参数估计
3. Parameter estimation using unsteady downwash model from real flight data of Hansa-3 aircraft [J] . R. Kumar, A. K. Ghosh The Aeronautical Journal . 2011,第1171期

机译：基于Hansa-3飞机实际飞行数据的非稳态下冲模型参数估计
4. ACCURACY CHARACTERISTICS ESTIMATION OF SNS DIFFERENTIAL MODE USED TO GET AIRCRAFT TRAJECTORY PARAMETERS DURING FLIGHT TESTS [C] . Kopelovich V., Polikarpov V., Kharin E., Saint Petersburg International Conference on Integrated Navigation Systems . 2005

机译：SNS差动模式的精度特性估计用于在飞行试验期间获得飞机轨迹参数
5. Flight testing of a remotely piloted vehicle for aircraft parameter estimation purposes. [D] . Seanor, Brad A. 2002

机译：出于飞机参数估计目的的遥控飞机的飞行测试。
6. Sample Size under Inverse Negative Binomial Group Testing for Accuracy in Parameter Estimation [O] . Osval Antonio Montesinos-López, Abelardo Montesinos-López, José Crossa, 2009

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7. Formulation of mathematical models using parameter estimation techniques and flight test data for the Bell 427 helicopter and the F/A-18 aircraft [O] . Nadeau-Beaulieu Michel 2007

机译：使用贝尔427直升机和F / a-18飞机的参数估算技术和飞行试验数据制定数学模型

ACCURACY CHARACTERISTICS ESTIMATION OF SNS DIFFERENTIAL MODE USED TO GET AIRCRAFT TRAJECTORY PARAMETERS DURING FLIGHT TESTS

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