🛰️航天仿真算法库 SpaceAST
0.0.1
载入中...
搜索中...
未找到
ScStateCalcEccentricity.hpp
浏览该文件的文档.
1
20
21
#pragma once
22
23
#include "AstGlobal.h"
24
#include "AstCore/ScStateCalcBodyRelated.hpp"
25
26
AST_NAMESPACE_BEGIN
27
33
class
AST_CORE_API
ScStateCalcEccentricity
:
public
ScStateCalcBodyRelated
34
{
35
public
:
36
AST_OBJECT(
ScStateCalcEccentricity
)
37
38
ScStateCalcEccentricity
() =
default
;
39
~ScStateCalcEccentricity
() =
default
;
40
public
:
41
errc_t calculate(
const
SpacecraftState
&scState,
double
& result)
override
;
42
};
43
44
45
46
49
AST_NAMESPACE_END
ast::ScStateCalcBodyRelated
定义
ScStateCalcBodyRelated.hpp:36
ast::ScStateCalcEccentricity
定义
ScStateCalcEccentricity.hpp:34
ast::SpacecraftState
航天器状态,包含轨道状态、质量、面积、阻力系数、光压、密度、压力、温度等属性
定义
SpacecraftState.hpp:38
src
AstCore
Orbit
Calculation
ScStateCalculation
KeplerianElements
ScStateCalcEccentricity.hpp
制作者
1.12.0