MATLAB Toolbox for simulating Single/Dual Frequency GPS and Carrier Phase Differential GPS
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Dual_Freq_GPS.asv
Dual_Freq_GPS.m
FlightMech_Model.asv
FlightMech_Model.m
MainGPS.asv
MainGPS.m
README.md
RK4_autopilot.asv
RK4_autopilot.m
atmosphere.m
autopilotplant.mat
body_to_ecef.m
calc_sat_pos_ecef.asv
calc_sat_pos_ecef.m
chistart.m
collect_phase_data.asv
collect_phase_data.m
collect_phase_data2.m
compute_distance.m
ecef_to_latlong.asv
ecef_to_latlong.m
enu_to_ecef.m
estimate_user_position_cdgps2.asv
estimate_user_position_cdgps2.m
eval_DOP.m
eval_Thrust.m
eval_aerod_coeff.asv
eval_aerod_coeff.m
eval_delay_iono.m
eval_delay_tropo.m
eval_el_az.m
eval_gaccel_body.asv
eval_gaccel_ned.m
eval_integer_ambiguity.m
eval_ned_to_ecef.m
eval_pr_measurement.asv
eval_pr_measurement.m
eval_sat_clock_offset.m
eval_sbas_correction.m
eval_state_derivative.asv
eval_state_derivative.m
gaccel_e.m
gps_alamanac_data.m
inres_pos.m
inres_pos_data.m
integ_RK4.asv
integ_RK4.m
landing_trajectory.mat
latlong_to_ecef.m
ned_to_ecef.m
newton_raphson.m
rcvr_clk_model.m
select_optimum_sats.asv
select_optimum_sats.m

README.md


License:

Software License Agreement (BSD License)

Copyright (c) 2013, Saurav Agarwal All rights reserved.

Redistribution and use in source and binary forms, with or without modification, are permitted provided that the following conditions are met:

  • Redistributions of source code must retain the above copyright notice, this list of conditions and the following disclaimer.
  • Redistributions in binary form must reproduce the above copyright notice, this list of conditions and the following disclaimer in the documentation and/or other materials provided with the distribution.
  • Neither the name of the Indian Institute of Technology, Bombay nor the names of its contributors may be used to endorse or promote products derived from this software without specific prior written permission.

THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT, INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING, BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE POSSIBILITY OF SUCH DAMAGE.

GPSMATLAB

MATLAB Toolbox for simulating Single/Dual Frequency GPS and Carrier Phase Differential GPS.

Contact

Visit: http://sauravag.com

References:

  1. S Agarwal and H B Hablani., “Automatic Aircraft Landing over Parabolic Trajectory using Precise GPS Measurements,” IJCA Proceedings on International Conference and workshop on Emerging Trends in Technology (ICWET) (7):38-45, 2011

  2. Agarwal, S. & Hablani, H.B., “Precise Positioning Using GPS for CAT-III Aircraft Operations Using Smoothed Pseudorange Measurements,” International Conference and Workshop on Emerging Trends in Technology, February 25-26, 2011, Mumbai, India