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

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

获取原文

页面导航

摘要
著录项
相似文献
相关主题

摘要

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：为了在飞行试验时获得飞机轨迹参数，实现实现卫星导航系统仪器（SNS）的差分操作模式使用。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。在各种飞行站点上导航参数准确性的估计是一项艰巨的任务。在该工作中，通过各种方法进行SNS差异模式的数据误差估计。

著录项

来源
《Saint Petersburg International Conference on Integrated Navigation Systems》|2005年||共3页
会议地点
作者
Kopelovich V.; Polikarpov V.; Kharin E.; Kopylov I.; Scientific Council of the Russian Academy of Sciences on the Problems of Motion Control and Navigation(RU); International Public Association-Academy of Navigation and Motion Control(ANMC); American Institute of Aeronautics and Astronautics(AIAA);
展开▼
作者单位

展开▼
会议组织
原文格式 PDF
正文语种
中图分类 V249.324-53;
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;测量参数测量的准确估计;

相似文献

外文文献
中文文献
专利

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

机译：飞机空气动力学特性的飞行试验估计-俄罗斯经验
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

机译：逆负二项式群检验下的样本量可提高参数估计的准确性
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

摘要

著录项

相似文献

相关主题

期刊订阅