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Differential equations of satellite motion
2022-06-29 15:02:00 【Obsession】
Satellite orbit differential equation :
The central force in satellite motion is a conservative force , The law of conservation of mechanical energy holds . therefore , We can use the total energy to discuss the specific form of satellite orbit . In the inverse square gravity problem , force The specific form of is known .
Because intentional force is conservative force , So there must be potential energy , Yes
(2) In style It is a quantity that has nothing to do with satellites but only with the earth , For the distance between the satellite and the earth , For satellite quality . Take the potential energy at infinity as zero , Then the distance between the particle and the force center is The gravitational potential energy is :
When we study the problem of mental force , Pictured 1 Shown , The law of conservation of mechanical energy and the law of conservation of moment of momentum are usually combined . The following two equations are commonly used as basic equations :

In the formula Is constant To unite and Type available :
In order to eliminate Type in the , Let's do the following transformation first :
take Into the Available :
take Jointly available :
figure out , And separate the variables and integrate to get :
The standard conic equation of the known polar coordinate system is :
Make ,, So you can put the formula Rewrite into The form of the formula . By the type You know , because The value of is always positive , So the total energy Determines the shape of the satellite orbit .
Let's discuss it in categories :
, be , The orbit is an ellipse ;
, be , The orbit is a parabola ;
, be , The orbit is hyperbolic .
Numerical simulation
1、 Circular orbit


2、 Elliptical orbit


3、 Parabolic orbit


3、 Hyperbolic orbit


This article is an original work , Reprint please contact the author :[email protected]
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