DetermineVArrival.m

版本 1.0.0.0 (2.1 KB) 作者: Brandon
Determine Arrival Velocity of a Orbiting Object
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更新时间 2014/5/19

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This function determines the arrival velocity of an orbit for a given initial position and velocity and arrival position
Inputs:
r1 - initial position
v1 - initial velocity
r2 - arrival position
mu - gravitational parameter
Outputs:
v2 - arrival velocity
The units of the input variables must agree. Examples include: (km & s),
(DU & TU), etc

引用格式

Brandon (2024). DetermineVArrival.m (https://www.mathworks.com/matlabcentral/fileexchange/46650-determinevarrival-m), MATLAB Central File Exchange. 检索时间: .

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1.0.0.0