卫星导航实验报告

Omega + 2*gpsPi, 2*gpsPi);Р Р %--- Compute satellite coordinates ------------------------------------Р satPositions(1, satNr) = cos(u)*r * cos(Omega) - sin(u)*r * cos(i)*sin(Omega);Р satPositions(2, satNr) = cos(u)*r * sin(Omega) + sin(u)*r * cos(i)*cos(Omega);Р satPositions(3, satNr) = sin(u)*r * sin(i);Р【结果记录与分析】Р按附表格式整理实验数据,并整理所编程序。(以一颗卫星为例)Р附表一Р卫星时间Р 卫星序号:10Р仰角РDoppler 频移Р解算坐标РECEF坐标Р308640Р-6898114.365083Р-6898114.840231Р69.366891°Р4.836185542725942 KHzР10231973.056976Р10231973.400231Р11426817.711968Р11426816.812402Р308641Р-6899460.241363Р-6899460.726453Р69. 366891°Р4.836197123663138 KHzР10232948.980243Р10232949.326035Р11424268.230451Р11424267.987032Р308642Р-6890805.435930Р-6890805.874032Р69. 366891°Р4.836208705610145 KHzР10233924.760354Р10233924.785343Р11421718.243299Р11421718.207653