文件名称:GlobalPositioningSystemsInertialNavigationanditegr
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This diskette (version 1.0) contains demonstration programs and source codes in MATLAB (v.5.2) for algorithms listed in the textbook Global Positioning Systems, Inertial Navigation, and Integration, by M. S. Grewal, Lawrence Weill, and A. P. Andrews, published by John Wiley and Sons, 2000.
Contents: MATLAB (Version 5.2) Demonstrations & scr ipts
Chapter4
ephemeris.m calculates the GPS satellite position in ECEF coordinates from its ephemeris parameters.
Chapter5
Klobuchar_fix.m calculates the ionospheric delay.
Chapter6 (shows the quaternion utilities)
Contents: MATLAB (Version 5.2) Demonstrations & scr ipts
Chapter4
ephemeris.m calculates the GPS satellite position in ECEF coordinates from its ephemeris parameters.
Chapter5
Klobuchar_fix.m calculates the ionospheric delay.
Chapter6 (shows the quaternion utilities)
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下载文件列表
压缩包 : 31767677globalpositioningsystemsinertialnavigationanditegration.rar 列表 Chapter3\ephemeris.m CHAPTER5\alma.dat CHAPTER5\Klobuchar_fix.m Chapter6\latitude.m Chapter6\quaternions\qmat2vec.m Chapter6\quaternions\quatmats.m Chapter6\quaternions\quattrim.m Chapter6\quaternions\qvec2mat.m Chapter6\quaternions\rotdemo.m Chapter6\quaternions\rotdemo1.m Chapter6\quaternions\rotdemo2.m Chapter6\quaternions\rotdemo3.m Chapter6\quaternions\rotvec2qvec.m Chapter6\quaternions\trimdemo.m Chapter6\quaternions\viewfrom.m Chapter6\quaternions\vrot2qrot.m Chapter6\quaternions Chapter3 CHAPTER5 Chapter6