%% 与ATk进行连接
%与ATK进行连接,IP地址请输入本机地址,示例中为127.0.0.1。端口号默认为6655
conID = atkOpen('127.0.0.1',6655);
%% 场景属性
%新建一个名为 InclinationChange 的场景
atkConnect(conID, 'New', '/ Scenario InclinationChange');
%使用UTCG格式设置场景分析时间段,开始时间为2022-11-05零点,结束时间为2022-11-08零点
atkConnect(conID, 'SetAnalysisTimePeriod', '* "5 Nov 2022 00:00:00.000" "8 Nov 2022 00:00:00.000" ');
%新建一个名为 SatInclinationChange 的卫星
atkConnect(conID, 'New', '/ Satellite SatInclinationChange');
%仿真重置
atkConnect(conID, 'Animate', '* Reset');
%% 卫星轨道属性
%设置卫星轨迹线宽为2
atkConnect(conID, 'Graphics', '*/Satellite/SatInclinationChange Basic LineWidth 2');
%设置卫星轨道预报器类型为机动规划;第一级目录默认存在一个初始段,一个预报段
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange SetProp');
%在第一级目录下添加一个预报段,默认段名为Propagate
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange InsertSegment MainSequence.SegmentList.- Propagate');
%在第一级目录下添加一个瞄准序列段,默认段名为Target_Sequence
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange InsertSegment MainSequence.SegmentList.- Target_Sequence');
%在瞄准序列段内添加一个机动段,默认段名为Maneuver
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange InsertSegment MainSequence.SegmentList.Target_Sequence.SegmentList.- Maneuver');
%在第一级目录下添加一个预报段;由于已经存在一个预报段,所以默认此段段名为Propagate1
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange InsertSegment MainSequence.SegmentList.- Propagate');
%在第一级目录下添加一个瞄准序列段;由于已经存在一个瞄准序列段,所以默认此段段名为Target_Sequence1
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange InsertSegment MainSequence.SegmentList.- Target_Sequence');
%在Target_Sequence1下添加一个机动段,默认段名为Maneuver
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange InsertSegment MainSequence.SegmentList.Target_Sequence1.SegmentList.- Maneuver');
%在第一级目录下添加一个预报段;由于已经存在两个预报段,所以默认此段段名为Propagate2
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange InsertSegment MainSequence.SegmentList.- Propagate');
%在第一级目录下添加一个瞄准序列段;由于已经存在两个瞄准序列段,所以默认此段段名为Target_Sequence2
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange InsertSegment MainSequence.SegmentList.- Target_Sequence');
%在Target_Sequence2下添加一个机动段,默认段名为Maneuver
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange InsertSegment MainSequence.SegmentList.Target_Sequence2.SegmentList.- Maneuver');
%在第一级目录下添加一个预报段;由于已经存在三个预报段,所以此段段名为Propagate3
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange InsertSegment MainSequence.SegmentList.- Propagate');
%设置初始段轨道历元
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange SetValue MainSequence.SegmentList.Initial_State.InitialState.Epoch 5 Nov 2022 00:00:00.000 UTCG');
%设置初始段坐标类型为轨道根数
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange SetValue MainSequence.SegmentList.Initial_State.CoordinateType "Modified Keplerian" ');
%设置初始段半长轴为6570000米
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange SetValue MainSequence.SegmentList.Initial_State.InitialState.Keplerian.sma 6570000 m');
%设置初始段偏心率为0
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange SetValue MainSequence.SegmentList.Initial_State.InitialState.Keplerian.ecc 0');
%设置初始段轨道倾角为28度
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange SetValue MainSequence.SegmentList.Initial_State.InitialState.Keplerian.inc 28 deg');
%设置初始段升交点赤经为0度
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange SetValue MainSequence.SegmentList.Initial_State.InitialState.Keplerian.RAAN 0');
%设置初始段近拱点角距为0度
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange SetValue MainSequence.SegmentList.Initial_State.InitialState.Keplerian.w 0');
%设置初始段真近点角为0度
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange SetValue MainSequence.SegmentList.Initial_State.InitialState.Keplerian.ta 0');
%设置第一个预报段颜色为红色
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange SetValue MainSequence.SegmentList.Propagate.SegmentColor 4278190335');
%设置第一个预报段停止条件为Duration
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange SetValue MainSequence.SegmentList.Propagate.StoppingConditions Duration');
%设置第一个预报段停止条件Duration的触发值为7200秒
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange SetValue MainSequence.SegmentList.Propagate.StoppingConditions.Duration.TripValue 7200 sec');
%设置第一个预报段停止条件Duration的误差值为0.0001秒
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange SetValue MainSequence.SegmentList.Propagate.StoppingConditions.Duration.Tolerance 0.0001 sec');
%设置第一个瞄准序列段内的机动段颜色
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange SetValue MainSequence.SegmentList.Target_Sequence.SegmentList.Maneuver.SegmentColor 4278212095');
%设置第一个瞄准序列段内的机动段在脉冲类型下推力坐标轴为VNC
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange SetValue MainSequence.SegmentList.Target_Sequence.SegmentList.Maneuver.ImpulsiveMnvr.ThrustAxes "Satellite VNC(Earth)" ');
%设置第一个瞄准序列段控制变量为机动段的直角坐标X
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange AddMCSSegmentControl MainSequence.SegmentList.Target_Sequence.SegmentList.Maneuver ImpulsiveMnvr.Cartesian.X');
%第一个瞄准序列段添加属性页
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange SetValue MainSequence.SegmentList.Target_Sequence.Profiles Differential_Corrector');
%设置第一个瞄准序列段的控制变量-机动段直角坐标X为使用状态
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange SetMCSControlValue MainSequence.SegmentList.Target_Sequence.Profiles.Differential_Corrector Maneuver ImpulsiveMnvr.Cartesian.X Active true');
%设置第一个瞄准序列段的控制变量-机动段直角坐标X的最大步长为100米每秒
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange SetMCSControlValue MainSequence.SegmentList.Target_Sequence.Profiles.Differential_Corrector Maneuver ImpulsiveMnvr.Cartesian.X MaxStep 100 m/sec');
%设置第一个瞄准序列段的控制变量-机动段直角坐标X的累计校正量为2456.42862556706米每秒
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange SetMCSControlValue MainSequence.SegmentList.Target_Sequence.Profiles.Differential_Corrector Maneuver ImpulsiveMnvr.Cartesian.X Correction 2456.42862556706 m/sec');
%设置第一个瞄准序列段的控制变量-机动段直角坐标X的摄动量为0.1米每秒
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange SetMCSControlValue MainSequence.SegmentList.Target_Sequence.Profiles.Differential_Corrector Maneuver ImpulsiveMnvr.Cartesian.X Perturbation 0.1 m/sec');
%设置第一个瞄准序列段的控制变量-机动段直角坐标X的归一化参数为0.1米每秒
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange SetMCSControlValue MainSequence.SegmentList.Target_Sequence.Profiles.Differential_Corrector Maneuver ImpulsiveMnvr.Cartesian.X Scale 1 m/sec');
%设置第一个瞄准序列段内的机动段的约束为Radius Of Apoapsis
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange SetValue MainSequence.SegmentList.Target_Sequence.SegmentList.Maneuver.Results " Radius Of Apoapsis " ');
%设置第一个瞄准序列段的机动段约束Radius Of Apoapsis为使用状态
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange SetMCSConstraintValue MainSequence.SegmentList.Target_Sequence.Profiles.Differential_Corrector Maneuver "Radius Of Apoapsis" Active true');
%设置第一个瞄准序列段的机动段约束Radius Of Apoapsis的收敛误差为0.1米
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange SetMCSConstraintValue MainSequence.SegmentList.Target_Sequence.Profiles.Differential_Corrector Maneuver "Radius Of Apoapsis" Tolerance 0.1 m');
%设置第一个瞄准序列段的机动段约束Radius Of Apoapsis的归一化参数为1米
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange SetMCSConstraintValue MainSequence.SegmentList.Target_Sequence.Profiles.Differential_Corrector Maneuver "Radius Of Apoapsis" Scale 1 m');
%设置第一个瞄准序列段的机动段约束Radius Of Apoapsis的权重系数为1
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange SetMCSConstraintValue MainSequence.SegmentList.Target_Sequence.Profiles.Differential_Corrector Maneuver "Radius Of Apoapsis" Weight 1');
%设置第一个瞄准序列段的机动段约束Radius Of Apoapsis的期望值为42160000米
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange SetMCSConstraintValue MainSequence.SegmentList.Target_Sequence.Profiles.Differential_Corrector Maneuver "Radius Of Apoapsis" Desired 42160000 m');
%设置第二个预报段的颜色为亮紫色
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange SetValue MainSequence.SegmentList.Propagate1.SegmentColor 4294902015');
%设置第二个预报段的停止条件为Apoapsis
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange SetValue MainSequence.SegmentList.Propagate1.StoppingConditions Apoapsis');
%设置第二个预报段停止条件Apoapsis的重复次数为1
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange SetValue MainSequence.SegmentList.Propagate1.StoppingConditions.Apoapsis.RepeatCount 1');
%设置第二个预报段停止条件Apoapsis的误差值为0.0001
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange SetValue MainSequence.SegmentList.Propagate1.StoppingConditions.Apoapsis.Tolerance 0.0001');
%设置第二个瞄准序列段的机动段颜色
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange SetValue MainSequence.SegmentList.Target_Sequence1.SegmentList.Maneuver.SegmentColor -256');
%设置第二个瞄准序列段内的机动段没冲类型下推力坐标轴为VNC
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange SetValue MainSequence.SegmentList.Target_Sequence1.SegmentList.Maneuver.ImpulsiveMnvr.ThrustAxes "Satellite VNC(Earth)" ');
%设置第二个瞄准序列段的控制变量为机动段直角坐标X
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange AddMCSSegmentControl MainSequence.SegmentList.Target_Sequence1.SegmentList.Maneuver ImpulsiveMnvr.Cartesian.X');
%第二个瞄准序列段添加属性页
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange SetValue MainSequence.SegmentList.Target_Sequence1.Profiles Differential_Corrector');
%设置第二个瞄准序列段的控制变量-机动段直角坐标X为使用状态
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange SetMCSControlValue MainSequence.SegmentList.Target_Sequence1.Profiles.Differential_Corrector Maneuver ImpulsiveMnvr.Cartesian.X Active true');
%设置第二个瞄准序列段的控制变量-机动段直角坐标X的最大步长为100米每秒
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange SetMCSControlValue MainSequence.SegmentList.Target_Sequence1.Profiles.Differential_Corrector Maneuver ImpulsiveMnvr.Cartesian.X MaxStep 100 m/sec');
%设置第二个瞄准序列段的控制变量-机动段直角坐标X的累计校正量为1480.06329844802 米每秒
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange SetMCSControlValue MainSequence.SegmentList.Target_Sequence1.Profiles.Differential_Corrector Maneuver ImpulsiveMnvr.Cartesian.X Correction 1480.06329844802 m/sec');
%设置第二个瞄准序列段的控制变量-机动段直角坐标X的摄动量为0.1米每秒
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange SetMCSControlValue MainSequence.SegmentList.Target_Sequence1.Profiles.Differential_Corrector Maneuver ImpulsiveMnvr.Cartesian.X Perturbation 0.1 m/sec');
%设置第二个瞄准序列段的控制变量-机动段直角坐标X的归一化参数为1米每秒
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange SetMCSControlValue MainSequence.SegmentList.Target_Sequence1.Profiles.Differential_Corrector Maneuver ImpulsiveMnvr.Cartesian.X Scale 1 m/sec');
%设置第二个瞄准序列段内的机动段约束为Eccentricity
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange SetValue MainSequence.SegmentList.Target_Sequence1.SegmentList.Maneuver.Results "Eccentricity" ');
%设置第二个瞄准序列段内的机动段约束Eccentricity为使用状态
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange SetMCSConstraintValue MainSequence.SegmentList.Target_Sequence1.Profiles.Differential_Corrector Maneuver "Eccentricity" Active true');
%设置第二个瞄准序列段内的机动段约束收敛误差为0.001
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange SetMCSConstraintValue MainSequence.SegmentList.Target_Sequence1.Profiles.Differential_Corrector Maneuver "Eccentricity" Tolerance 0.001');
%设置第二个瞄准序列段内的机动段约束归一化参数为1
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange SetMCSConstraintValue MainSequence.SegmentList.Target_Sequence1.Profiles.Differential_Corrector Maneuver "Eccentricity" Scale 1');
%设置第二个瞄准序列段内的机动段约束权重系数为1
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange SetMCSConstraintValue MainSequence.SegmentList.Target_Sequence1.Profiles.Differential_Corrector Maneuver "Eccentricity" Weight 1');
%设置第二个瞄准序列段内的机动段约束期望值为0
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange SetMCSConstraintValue MainSequence.SegmentList.Target_Sequence1.Profiles.Differential_Corrector Maneuver "Eccentricity" Desired 0');
%设置第三个预报段的颜色为绿色
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange SetValue MainSequence.SegmentList.Propagate2.SegmentColor 4278255360');
%设置第三个预报段的停止条件为AscendingNode
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange SetValue MainSequence.SegmentList.Propagate2.StoppingConditions AscendingNode');
%设置第三个预报段的停止条件AscendingNode的重复次数为2
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange SetValue MainSequence.SegmentList.Propagate2.StoppingConditions.AscendingNode.RepeatCount 2');
%设置第三个预报段的停止条件AscendingNode的误差值为0.000001
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange SetValue MainSequence.SegmentList.Propagate2.StoppingConditions.AscendingNode.Tolerance 0.000001');
%设置第三个瞄准序列段的机动段颜色
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange SetValue MainSequence.SegmentList.Target_Sequence2.SegmentList.Maneuver.SegmentColor -65536');
%设置第三个瞄准序列段内的机动段脉冲属性下推力坐标轴为VNC
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange SetValue MainSequence.SegmentList.Target_Sequence2.SegmentList.Maneuver.ImpulsiveMnvr.ThrustAxes "Satellite VNC(Earth)" ');
%设置第三个瞄准序列段的控制变量为机动段的直角坐标X
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange AddMCSSegmentControl MainSequence.SegmentList.Target_Sequence2.SegmentList.Maneuver Impul-siveMnvr.Cartesian.X');
%第三个瞄准序列段添加属性页
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange SetValue MainSequence.SegmentList.Target_Sequence2.Profiles Differential_Corrector');
%设置第三个瞄准序列段控制变量-机动段直角坐标X为使用状态
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange SetMCSControlValue MainSequence.SegmentList.Target_Sequence2.Profiles.Differential_Corrector Maneuver ImpulsiveMnvr.Cartesian.X Active true');
%设置第三个瞄准序列段控制变量-机动段直角坐标X的最大步长为100米每秒
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange SetMCSControlValue MainSequence.SegmentList.Target_Sequence2.Profiles.Differential_Corrector Maneuver ImpulsiveMnvr.Cartesian.X MaxStep 100 m/sec');
%设置第三个瞄准序列段控制变量-机动段直角坐标X的累计校正量为-359.983751789857米每秒
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange SetMCSControlValue MainSequence.SegmentList.Target_Sequence2.Profiles.Differential_Corrector Maneuver ImpulsiveMnvr.Cartesian.X Correction -359.983751789857 m/sec');
%设置第三个瞄准序列段控制变量-机动段直角坐标X摄动量为0.1米每秒
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange SetMCSControlValue MainSequence.SegmentList.Target_Sequence2.Profiles.Differential_Corrector Maneuver ImpulsiveMnvr.Cartesian.X Perturbation 0.1 m/sec');
%设置第三个瞄准序列段控制变量-机动段直角坐标X归一化参数为1米每秒
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange SetMCSControlValue MainSequence.SegmentList.Target_Sequence2.Profiles.Differential_Corrector Maneuver ImpulsiveMnvr.Cartesian.X Scale 1 m/sec');
%设置第三个瞄准序列段的控制变量为机动段直角坐标Y
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange AddMCSSegmentControl MainSequence.SegmentList.Target_Sequence2.SegmentList.Maneuver Impul-siveMnvr.Cartesian.Y');
%设置第三个瞄准序列段控制变量-机动段直角坐标Y为使用状态
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange SetMCSControlValue MainSequence.SegmentList.Target_Sequence2.Profiles.Differential_Corrector Maneuver ImpulsiveMnvr.Cartesian.Y Active true');
%设置第三个瞄准序列段控制变量-机动段直角坐标Y的最大步长为100米每秒
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange SetMCSControlValue MainSequence.SegmentList.Target_Sequence2.Profiles.Differential_Corrector Maneuver ImpulsiveMnvr.Cartesian.Y MaxStep 100 m/sec');
%设置第三个瞄准序列段控制变量-机动段直角坐标Y的累计校正量为-1444.72488992759米每秒
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange SetMCSControlValue MainSequence.SegmentList.Target_Sequence2.Profiles.Differential_Corrector Maneuver ImpulsiveMnvr.Cartesian.Y Correction -1444.72488992759 m/sec');
%设置第三个瞄准序列段控制变量-机动段直角坐标Y的摄动量为0.1米每秒
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange SetMCSControlValue MainSequence.SegmentList.Target_Sequence2.Profiles.Differential_Corrector Maneuver ImpulsiveMnvr.Cartesian.Y Perturbation 0.1 m/sec');
%设置第三个瞄准序列段控制变量-机动段直角坐标Y的归一化参数为1米每秒
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange SetMCSControlValue MainSequence.SegmentList.Target_Sequence2.Profiles.Differential_Corrector Maneuver ImpulsiveMnvr.Cartesian.Y Scale 1 m/sec');
%设置第三个瞄准序列段内的机动段约束为Inclination和Eccentricity
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange SetValue MainSequence.SegmentList.Target_Sequence2.SegmentList.Maneuver.Results "Inclination" "Eccentricity" ');
%设置第三个瞄准序列段内机动段约束Inclination为使用状态
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange SetMCSConstraintValue MainSequence.SegmentList.Target_Sequence2.Profiles.Differential_Corrector Maneuver "In-clination" Active true');
%设置第三个瞄准序列段内机动段约束Inclination的收敛误差为0度
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange SetMCSConstraintValue MainSequence.SegmentList.Target_Sequence2.Profiles.Differential_Corrector Maneuver "In-clination" Tolerance 0 deg');
%设置第三个瞄准序列段内机动段约束Inclination的归一化参数为1弧度
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange SetMCSConstraintValue MainSequence.SegmentList.Target_Sequence2.Profiles.Differential_Corrector Maneuver "In-clination" Scale 1 rad');
%设置第三个瞄准序列段内机动段约束Inclination的权重系数为1
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange SetMCSConstraintValue MainSequence.SegmentList.Target_Sequence2.Profiles.Differential_Corrector Maneuver "In-clination" Weight 1');
%设置第三个瞄准序列段内机动段约束Inclination的期望值为0度
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange SetMCSConstraintValue MainSequence.SegmentList.Target_Sequence2.Profiles.Differential_Corrector Maneuver "In-clination" Desired 0 deg');
%设置第三个瞄准序列段内机动段约束Eccentricity为使用状态
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange SetMCSConstraintValue MainSequence.SegmentList.Target_Sequence2.Profiles.Differential_Corrector Maneuver "Eccentricity" Active true');
%设置第三个瞄准序列段内机动段约束Eccentricity的收敛误差为0.001
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange SetMCSConstraintValue MainSequence.SegmentList.Target_Sequence2.Profiles.Differential_Corrector Maneuver "Eccentricity" Tolerance 0.001');
%设置第三个瞄准序列段内机动段约束Eccentricity的收敛误差为0.001
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange SetMCSConstraintValue MainSequence.SegmentList.Target_Sequence2.Profiles.Differential_Corrector Maneuver "Eccentricity" Scale 1');
%设置第三个瞄准序列段内机动段约束Eccentricity的权重系数为1
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange SetMCSConstraintValue MainSequence.SegmentList.Target_Sequence2.Profiles.Differential_Corrector Maneuver "Eccentricity" Weight 1');
%设置第三个瞄准序列段内机动段约束Eccentricity期望值为0
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange SetMCSConstraintValue MainSequence.SegmentList.Target_Sequence2.Profiles.Differential_Corrector Maneuver "Eccentricity" Desired 0');
%设置第四个预报段的颜色为黄色
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange SetValue MainSequence.SegmentList.Propagate3.SegmentColor 4278255615');
%设置第四个预报段的停止条件为Duration
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange SetValue MainSequence.SegmentList.Propagate3.StoppingConditions Duration');
%设置第四个预报段停止条件Duration的触发值为129600秒
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange SetValue MainSequence.SegmentList.Propagate3.StoppingConditions.Duration.TripValue 129600 sec');
%设置第四个预报段停止条件Duration的误差值为0.00001秒
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange SetValue MainSequence.SegmentList.Propagate3.StoppingConditions.Duration.Tolerance 0.00001 sec');
%运行此算例
atkConnect(conID, 'Astrogator', '*/Satellite/SatInclinationChange RunMCS');
根据此语句,帮我写多个卫星通过优化蚁群算法和DE算法变轨去捕捉多个空间碎片目标的Matlab程序,尽量详细具体,不要省略步骤
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