代码搜索：performs
找到约 4,693 项符合「performs」的源代码
代码结果 4,693
www.eeworm.com/read/419474/10866111
m venugd.m
% venugd.m
% Scope: This MATLAB macro performs the transformation from ENU (East,
% North, Up) to geodetic coordinates for a given position vector
%
www.eeworm.com/read/419474/10866140
m veciecef.m
% veciecef.m
% Scope: This MATLAB macro performs the transformation from ECI (Earth
% Centered Inertial) to ECEF coordinates for a given position vector
%
www.eeworm.com/read/419474/10866194
m venuecef.m
% venuecef.m
% Scope: This MATLAB macro performs the transformation from ENU (East,
% North, Up) to ECEF coordinates for a given position vector and
%
www.eeworm.com/read/419474/10866209
m tecefgd2.m
% tecefgd2.m
% Scope: This MATLAB macro performs the transformation from ECEF to geodetic
% coordinates for a given position by using an iterative process;
www.eeworm.com/read/419474/10866239
m vgdenu.m
% vgdenu.m
% Scope: This MATLAB macro performs the transformation from geodetic to
% ENU (East, North, Up) coordinates for a given position vector
%
www.eeworm.com/read/419474/10866269
m vecefeci.m
% vecefeci.m
% Scope: This MATLAB macro performs the transformation from ECEF to ECI
% (Earth Centered Inertial) coordinates for a given position vector
%
www.eeworm.com/read/455057/7378374
m acquisitionconvolution.m
function [codephase,frequency] = acquisitionConvolution(svnum)
% Performs acquisition on collected data
% Searches for the satellite with number svnum
% Returns the code phase and the coarse frequency
www.eeworm.com/read/437241/7753113
sh bkora.sh
#####################################################################
set -x
# PROGRAM NAME:coldbackup_ux
# PURPOSE:Performs cold backup of the database. Database
#should be online when you
www.eeworm.com/read/436995/7757298
m venugd.m
% venugd.m
% Scope: This MATLAB macro performs the transformation from ENU (East,
% North, Up) to geodetic coordinates for a given position vector
%
www.eeworm.com/read/436995/7757324
m veciecef.m
% veciecef.m
% Scope: This MATLAB macro performs the transformation from ECI (Earth
% Centered Inertial) to ECEF coordinates for a given position vector
%