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基于单天线GPS载波幅度的旋转载体滚转角测量 被引量:6

Single Antenna GPS Carrier Amplitude Based Rolling Angle Determination of Spinning Vehicle
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摘要 传统的载体滚转角和转速测量方法成本高昂且仅限于高价值平台,为降低成本利用GPS信号测量滚转角的方法日益受到关注。将GPS载波信号的相位和幅度信息用于姿态测量,是目前旋转平台基于GPS测姿的两类主要方法。为了实现旋转载体的低成本高精度滚转角和转速测量,本文提出了单天线结构的利用GPS卫星接收机硬件相关器直接输出的导航用载波I/Q信号幅度特性,设计基于EKF的滚转角滤波器,利用载波I/Q信号的幅度特性对载波频率进行估计与跟踪,从而实现旋转载体的滚转角和转速的精确计算。实测数据试验表明,对于旋转载体仅利用卫星载波I/Q信号的幅度信息,本文提出的算法即可实时计算出旋转载体的滚转角和转速,且计算精度能够满足大多数的实际工程应用。 Traditional rolling angle and rolling rate measurement are costly and merely applied by high value plat-forms. In order to reduce cost, rolling angle determination method based on GPS signal is put forward. Rolling an-gle measurement by using GPS carrier phase and amplitude are the two main techniques used for attitude determina-tion. An approach to achieve high precision measurement of rolling angle and rolling rate of spinning vehicle with low cost is presented, that is, directly obtain I/Q signal amplitude signature of carrier for navigation by using single antenna GPS satellite receiver hardware correlator, and a rolling angle filter based on extended Kalman filtering ( EKF) is designed to estimate and track carrier frequency by using amplitude signature of carrier I/Q signals, so as to calculate rolling angle and rolling rate of spinning vehicle precisely. Actual test results show that, for using only amplitude information of I/Q signals, rolling rate and rolling angle of spinning vehicle can be calculated in real-time by using proposed method, and calculation accuracy can meet requirements of most practical applications.
出处 《火控雷达技术》 2014年第3期6-11,16,共7页 Fire Control Radar Technology
关键词 单天线 滚转角 载波幅度 旋转载体 滚转计算 single antenna roll angle carrier amplitude spinning vehicle rolling determination
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  • 1M. Campo- Cossio, A. Puras, R. Arnau, D. Bolado, Real- time attitude determination sys- tem based on GPS carrier phase measurements and aided by low -cost inertial sensors for high dynamic applications[C]. 13th lAIN world con- gress and exhibition, Sweden, 2009,27 - 29.
  • 2Cohen, C. E. , and Parkinson, B.W. Integer Ambiguity Resolution of the GPS Carrier for Spacecraft Attitude Determination [ J]. AIAA, 2010, 2(19) :519 -537.
  • 3Bahder, Thomas B. Attitude Determina- tion from Single - Antenna Carrier - Phase Measurements[ J]. Journal of Applied Physics. 2002, 91 (7) :4677 -4684.
  • 4Alfred H. Krall and Thomas B. Bahder. Orientation and velocity effects in the global po- sitioning system [ J ]. Journal of Applied Phys- ics. 2001, 90(12) :6513 -6525.
  • 5Steven B. Alexander, Richard Redhead. Systems and Methods for Determining a Rota- tional Position of an Object [ P]. US. Patent,US 20100052981 A1, 2010.
  • 6James H. Doizy, Gary A. McGraw. Spinning- Vehicle Navigation Using Apparent Modulation of Navigational Signals [ P]. US. Patent, US 6520448 B1, 2003.
  • 7Jianhui Luo, Wallace E. VandZr Velde, et al. Single Antenna GPS Measurement of Roll Rate and Roll Angle of Spinning Vehicle [ P]. US. Patent, Pub. No. US 20130169477 A1, 2013.
  • 8Leandro Baroni and Helio Koiti Kuga. Analysis of Attitude Determination Methods U- sing GPS Carrier Phase Measurements [ M ]. Hindawi Publishing Corporation Mathematical Problems in Engineering. 2012,1 - 10.

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