🛰️航天仿真算法库 SpaceAST
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AttitudeMissile.hpp
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#pragma once
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#include "AstGlobal.h"
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#include "
AttitudeTrajectoryRelated.hpp
"
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AST_NAMESPACE_BEGIN
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class
AST_CORE_API
AttitudeMissile
:
public
AttitudeTrajectoryRelated
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{
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public
:
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AST_OBJECT(
AttitudeMissile
)
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AttitudeMissile
() =
default
;
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AttitudeMissile
(
Point
* point,
Body
* body);
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~AttitudeMissile
()
override
=
default
;
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public
:
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errc_t
getTransform
(
const
TimePoint
& tp,
Rotation
& rotation)
const override
;
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errc_t
getTransform
(
const
TimePoint
& tp,
KinematicRotation
& rotation)
const override
;
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private
:
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// 屏蔽父类的 setFrame 方法
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void
setFrame(
Frame
* frame) =
delete
;
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public
:
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void
setBody(
Body
* body);
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};
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AST_NAMESPACE_END
AttitudeTrajectoryRelated.hpp
ast::AttitudeMissile
ECI 速度对齐 + 对地约束姿态
定义
AttitudeMissile.hpp:39
ast::AttitudeTrajectoryRelated
与轨迹相关的姿态
定义
AttitudeTrajectoryRelated.hpp:40
ast::Axes::getTransform
virtual errc_t getTransform(const TimePoint &tp, Rotation &rotation) const =0
获取当前轴系相对于父轴系的旋转变换
ast::CelestialBody
天体
定义
CelestialBody.hpp:72
ast::Frame
坐标系抽象基类
定义
Frame.hpp:74
ast::KinematicRotation
运动学坐标系旋转
定义
KinematicRotation.hpp:50
ast::Point
点抽象基类
定义
Point.hpp:42
ast::Rotation
坐标系旋转类
定义
Rotation.hpp:55
ast::TimePoint
绝对时间点
定义
TimePoint.hpp:108
src
AstCore
Attitude
AttitudeMissile.hpp
制作者
1.12.0