Rocket_Trajectory_Calculator-master
所属分类：仿真建模
开发工具：C/C++
文件大小：16KB
下载次数：1
上传日期：2021-04-12 16:37:20
上 传 者：
woerjiade
说明： 使用火箭发动机的等熵一维可压缩流近似值，使用电动机和气压条件计算火箭的三维轨迹。计算阻力时要考虑可压缩流量。
(The three-dimensional trajectory of the rocket is calculated by using the isentropic one-dimensional compressible flow approximation of the rocket engine and the motor and air pressure conditions. Compressible flow should be considered when calculating resistance. Work in process)
文件列表:
TrajectorySim (0, 2016-01-07)
TrajectorySim\Calculator.cpp (6140, 2016-01-07)
TrajectorySim\Calculator.h (1374, 2016-01-07)
TrajectorySim\Environment.cpp (1092, 2016-01-07)
TrajectorySim\Environment.h (448, 2016-01-07)
TrajectorySim\Euler.cpp (287, 2016-01-07)
TrajectorySim\Euler.h (228, 2016-01-07)
TrajectorySim\GaussianQuad.cpp (1971, 2016-01-07)
TrajectorySim\GaussianQuad.h (445, 2016-01-07)
TrajectorySim\KalmanFilter.cpp (1147, 2016-01-07)
TrajectorySim\KalmanFilter.h (1193, 2016-01-07)
TrajectorySim\Quaternion.cpp (2977, 2016-01-07)
TrajectorySim\Quaternion.h (597, 2016-01-07)
TrajectorySim\Vec3D.cpp (1589, 2016-01-07)
TrajectorySim\Vec3D.h (596, 2016-01-07)
TrajectorySim\Vector.cpp (2491, 2016-01-07)
TrajectorySim\Vector.h (1495, 2016-01-07)
TrajectorySim\Vehicle.cpp (1701, 2016-01-07)
TrajectorySim\Vehicle.h (1456, 2016-01-07)
TrajectorySim\main.cpp (1068, 2016-01-07)
# Davidthefat-Rocket_Trajectory_Calculator
Calculates 3D trajectory of rocket using motor and barometric conditions using isentropic 1D compressible flow approximation of rocket motor. Compressible flow is taken into account for drag calculations.
WIP
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