Analysis performed: 19-Jun-2008 09:05:12
| File Name | Size | Last Modified Date | Will be Exported |
|---|---|---|---|
| C:\work\Simulink2007Tour\LunarEx\CEV\SourceFiles\CEV.bmp (open) | 494262 bytes | 2007-08-27 16:54:44 | true |
| C:\work\Simulink2007Tour\LunarEx\CEV\SourceFiles\Lander_Moon180_1.wrl (open) | 5748 bytes | 2007-09-25 16:28:14 | true |
| C:\work\Simulink2007Tour\LunarEx\CEV\SourceFiles\LSAM_Ascent.bmp (open) | 1304182 bytes | 2007-09-17 18:16:40 | true |
| C:\work\Simulink2007Tour\LunarEx\CEV\SourceFiles\LSAM_Descent.bmp (open) | 984490 bytes | 2007-08-27 17:01:24 | true |
| C:\work\Simulink2007Tour\LunarEx\CEV\SourceFiles\Lunar_Mission.mdl (open) | 155758 bytes | 2007-10-03 12:21:54 | true |
| C:\work\Simulink2007Tour\LunarEx\CEV\SourceFiles\actuator.JPG (open) | 158924 bytes | 2007-08-28 16:30:42 | true |
| C:\work\Simulink2007Tour\LunarEx\CEV\SourceFiles\GNC.JPG (open) | 78208 bytes | 2007-08-29 12:14:54 | true |
| C:\work\Simulink2007Tour\LunarEx\CEV\SourceFiles\sensor.JPG (open) | 53495 bytes | 2007-08-29 12:15:36 | true |
| C:\work\Simulink2007Tour\LunarEx\CEV\SourceFiles\Spacecraft.mdl (open) | 506903 bytes | 2007-09-21 11:46:18 | true |
| C:\work\Simulink2007Tour\LunarEx\CEV\SourceFiles\Gimbal_Actuators.mdl (open) | 27848 bytes | 2007-08-20 16:08:38 | true |
| C:\work\Simulink2007Tour\LunarEx\CEV\SourceFiles\Spacecraft_Library.mdl (open) | 102119 bytes | 2007-09-01 09:12:08 | true |
Use the table below to determine where in a model a dependence upon a particular file or toolbox originates.
| Reference Type | Reference Location | File Name | Toolbox |
|---|---|---|---|
| ModelReference | Lunar_Mission/Lunar Lander Descent/Model (show) | C:\work\Simulink2007Tour\LunarEx\CEV\SourceFiles\Spacecraft.mdl (open) | (not in a toolbox) |
| LibraryLink | Lunar_Mission/Lunar Lander Ascent/6DoF (Quaternion) - Use As Point Mass (show) | C:\Program Files\MATLAB\R2008a\toolbox\aeroblks\aeroblks\aerolib6dof2.mdl (open) | Aerospace Blockset (3.1) |
| LibraryLink | Lunar_Mission/VR Data/Rotation Matrix to VRML Rotation (show) | C:\Program Files\MATLAB\R2008a\toolbox\vr\vr\vrlib.mdl (open) | Virtual Reality Toolbox (4.7) |
| LibraryLink | Lunar_Mission/VR Data/Rotation Matrix to VRML Rotation1 (show) | C:\Program Files\MATLAB\R2008a\toolbox\vr\vr\vrlib.mdl (open) | Virtual Reality Toolbox (4.7) |
| LibraryLink | Lunar_Mission/VR Sim (show) | C:\Program Files\MATLAB\R2008a\toolbox\vr\vr\vrlib.mdl (open) | Virtual Reality Toolbox (4.7) |
| Stateflow | Lunar_Mission/Lunar Lander and CEV Trajectory/Stateflow Calculation of Trajectory (show) | C:\Program Files\MATLAB\R2008a\toolbox\stateflow\stateflow\sf_sfun.mexw32 (open) | Stateflow (7.1) |
| Stateflow | Lunar_Mission/Mission Scheduler (show) | C:\Program Files\MATLAB\R2008a\toolbox\stateflow\stateflow\sf_sfun.mexw32 (open) | Stateflow (7.1) |
| SFunction | Lunar_Mission/Lunar Lander Ascent/Compute |r|^2/Dot Product (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\fixedandfloat\sfix_dot.mexw32 (open) | Simulink (7.1) |
| SFunction | Lunar_Mission/VR Sim (show) | C:\Program Files\MATLAB\R2008a\toolbox\vr\vr\vrsfunc.mexw32 (open) | Virtual Reality Toolbox (4.7) |
| SFunction | Lunar_Mission/Lunar Lander Ascent/Compute |r|^2/Dot Product (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\fixedandfloat\tlc_c\sfix_dot.tlc (open) | Simulink (7.1) |
| SourceBlock,VRWorldFile | Lunar_Mission/VR Sim (show) | C:\work\Simulink2007Tour\LunarEx\CEV\SourceFiles\Lander_Moon180_1.wrl (open) | (not in a toolbox) |
| BlockCallback,MaskInitialization | Lunar_Mission/Lunar Lander Ascent/6DoF (Quaternion) - Use As Point Mass (show) | C:\Program Files\MATLAB\R2008a\toolbox\aeroblks\aeroblks\aeroicon.m (open) | Aerospace Blockset (3.1) |
| BlockCallback,MaskInitialization | Lunar_Mission/Lunar Lander Ascent/6DoF (Quaternion) - Use As Point Mass (show) | C:\Program Files\MATLAB\R2008a\toolbox\aeroblks\aeroblks\aeroimage.m (open) | Aerospace Blockset (3.1) |
| BlockCallback,MaskDisplay | Lunar_Mission/Lunar Lander Ascent (show) | C:\Program Files\MATLAB\R2008a\toolbox\matlab\imagesci\imread.m (open) | MATLAB (7.6) |
| BlockCallback,MaskDisplay | Lunar_Mission/Lunar Lander Descent (show) | C:\Program Files\MATLAB\R2008a\toolbox\matlab\imagesci\imread.m (open) | MATLAB (7.6) |
| BlockCallback,MaskDisplay | Lunar_Mission/Lunar Lander and CEV Trajectory (show) | C:\Program Files\MATLAB\R2008a\toolbox\matlab\imagesci\imread.m (open) | MATLAB (7.6) |
| BlockCallback,MaskDisplay | Lunar_Mission/VR Sim (show) | C:\Program Files\MATLAB\R2008a\toolbox\matlab\imagesci\imread.m (open) | MATLAB (7.6) |
| BlockCallback,CloseFcn | Lunar_Mission/Subsystem/Landing (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\simulink\tagdialog.m (open) | Simulink (7.1) |
| BlockCallback,CloseFcn | Lunar_Mission/VR Data/From1 (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\simulink\tagdialog.m (open) | Simulink (7.1) |
| BlockCallback,CloseFcn | Lunar_Mission/VR Data/From2 (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\simulink\tagdialog.m (open) | Simulink (7.1) |
| BlockCallback,CloseFcn | Lunar_Mission/VR Data/From3 (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\simulink\tagdialog.m (open) | Simulink (7.1) |
| BlockCallback,CloseFcn | Lunar_Mission/VR Data/From4 (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\simulink\tagdialog.m (open) | Simulink (7.1) |
| BlockCallback,CloseFcn | Lunar_Mission/VR Data/From6 (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\simulink\tagdialog.m (open) | Simulink (7.1) |
| BlockCallback,CloseFcn | Lunar_Mission/VR Data/From7 (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\simulink\tagdialog.m (open) | Simulink (7.1) |
| BlockCallback,MaskDisplay | Lunar_Mission/VR Sim (show) | C:\Program Files\MATLAB\R2008a\toolbox\vr\vr\vrblockicon.png (open) | Virtual Reality Toolbox (4.7) |
| BlockCallback,CloseFcn | Lunar_Mission/VR Sim (show) | C:\Program Files\MATLAB\R2008a\toolbox\vr\vr\vrmfunc.m (open) | Virtual Reality Toolbox (4.7) |
| BlockCallback,CopyFcn | Lunar_Mission/VR Sim (show) | C:\Program Files\MATLAB\R2008a\toolbox\vr\vr\vrmfunc.m (open) | Virtual Reality Toolbox (4.7) |
| BlockCallback,DeleteFcn | Lunar_Mission/VR Sim (show) | C:\Program Files\MATLAB\R2008a\toolbox\vr\vr\vrmfunc.m (open) | Virtual Reality Toolbox (4.7) |
| BlockCallback,DestroyFcn | Lunar_Mission/VR Sim (show) | C:\Program Files\MATLAB\R2008a\toolbox\vr\vr\vrmfunc.m (open) | Virtual Reality Toolbox (4.7) |
| BlockCallback,InitFcn | Lunar_Mission/VR Sim (show) | C:\Program Files\MATLAB\R2008a\toolbox\vr\vr\vrmfunc.m (open) | Virtual Reality Toolbox (4.7) |
| BlockCallback,LoadFcn | Lunar_Mission/VR Sim (show) | C:\Program Files\MATLAB\R2008a\toolbox\vr\vr\vrmfunc.m (open) | Virtual Reality Toolbox (4.7) |
| BlockCallback,MaskInitialization | Lunar_Mission/VR Sim (show) | C:\Program Files\MATLAB\R2008a\toolbox\vr\vr\vrmfunc.m (open) | Virtual Reality Toolbox (4.7) |
| BlockCallback,OpenFcn | Lunar_Mission/VR Sim (show) | C:\Program Files\MATLAB\R2008a\toolbox\vr\vr\vrmfunc.m (open) | Virtual Reality Toolbox (4.7) |
| BlockCallback,PreSaveFcn | Lunar_Mission/VR Sim (show) | C:\Program Files\MATLAB\R2008a\toolbox\vr\vr\vrmfunc.m (open) | Virtual Reality Toolbox (4.7) |
| BlockCallback,StartFcn | Lunar_Mission/VR Sim (show) | C:\Program Files\MATLAB\R2008a\toolbox\vr\vr\vrmfunc.m (open) | Virtual Reality Toolbox (4.7) |
| BlockCallback,StopFcn | Lunar_Mission/VR Sim (show) | C:\Program Files\MATLAB\R2008a\toolbox\vr\vr\vrmfunc.m (open) | Virtual Reality Toolbox (4.7) |
| BlockCallback,MaskDisplay | Lunar_Mission/Lunar Lander and CEV Trajectory (show) | C:\work\Simulink2007Tour\LunarEx\CEV\SourceFiles\CEV.bmp (open) | (not in a toolbox) |
| BlockCallback,MaskDisplay | Lunar_Mission/Lunar Lander Ascent (show) | C:\work\Simulink2007Tour\LunarEx\CEV\SourceFiles\LSAM_Ascent.bmp (open) | (not in a toolbox) |
| BlockCallback,MaskDisplay | Lunar_Mission/Lunar Lander Descent (show) | C:\work\Simulink2007Tour\LunarEx\CEV\SourceFiles\LSAM_Descent.bmp (open) | (not in a toolbox) |
| LibraryLink | Spacecraft/Equations of Motion/Quaternion and Spacecraft Rotational Dynamics/3x3 cross product1 (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\simdemos\aerospace\aerospace.mdl (open) | Simulink (7.1) |
| LibraryLink | Spacecraft/Equations of Motion/Quaternion and Spacecraft Rotational Dynamics/q cross omega1 (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\simdemos\aerospace\aerospace.mdl (open) | Simulink (7.1) |
| LibraryLink | Spacecraft/GN&C Subsystem/Inertial System (Strapdown)/Quaternion Estimate from Measured Rates/Magnitude of q (show) | C:\Program Files\MATLAB\R2008a\toolbox\aeroblks\aeroblks\aerolibutil.mdl (open) | Aerospace Blockset (3.1) |
| LibraryLink | Spacecraft/GN&C Subsystem/Inertial System (Strapdown)/Quaternion Estimate from Measured Rates/q_1 cross omeqa (show) | C:\Program Files\MATLAB\R2008a\toolbox\aeroblks\aeroblks\aerolibutil.mdl (open) | Aerospace Blockset (3.1) |
| LibraryLink | Spacecraft/GN&C Subsystem/Inertial System (Strapdown)/Transformation Quaternion2DCM (show) | C:\work\Simulink2007Tour\LunarEx\CEV\SourceFiles\Spacecraft_Library.mdl (open) | (not in a toolbox) |
| LibraryLink | Spacecraft/Strap Down Sensors (Body Coords)/Strap Down Accelerometers/w x (w x d)/w x (w x d) (show) | C:\Program Files\MATLAB\R2008a\toolbox\aeroblks\aeroblks\aerolibutil.mdl (open) | Aerospace Blockset (3.1) |
| LibraryLink | Spacecraft/Strap Down Sensors (Body Coords)/Strap Down Accelerometers/w x (w x d)/w x d (show) | C:\Program Files\MATLAB\R2008a\toolbox\aeroblks\aeroblks\aerolibutil.mdl (open) | Aerospace Blockset (3.1) |
| LibraryLink | Spacecraft/Strap Down Sensors (Body Coords)/Strap Down Accelerometers/wdot x d (show) | C:\Program Files\MATLAB\R2008a\toolbox\aeroblks\aeroblks\aerolibutil.mdl (open) | Aerospace Blockset (3.1) |
| LibraryLink | Spacecraft/Actuators/Gimbal Actuator (Configurable) (show) | C:\work\Simulink2007Tour\LunarEx\CEV\SourceFiles\Gimbal_Actuators.mdl (open) | (not in a toolbox) |
| SFunction | Spacecraft/Actuators/Reaction Jets/Dot Product (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\fixedandfloat\sfix_dot.mexw32 (open) | Simulink (7.1) |
| SFunction | Spacecraft/Actuators/Reaction Jets/Dot Product1 (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\fixedandfloat\sfix_dot.mexw32 (open) | Simulink (7.1) |
| SFunction | Spacecraft/Actuators/Reaction Jets/Dot Product10 (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\fixedandfloat\sfix_dot.mexw32 (open) | Simulink (7.1) |
| SFunction | Spacecraft/Actuators/Reaction Jets/Dot Product11 (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\fixedandfloat\sfix_dot.mexw32 (open) | Simulink (7.1) |
| SFunction | Spacecraft/Actuators/Reaction Jets/Dot Product2 (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\fixedandfloat\sfix_dot.mexw32 (open) | Simulink (7.1) |
| SFunction | Spacecraft/Actuators/Reaction Jets/Dot Product3 (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\fixedandfloat\sfix_dot.mexw32 (open) | Simulink (7.1) |
| SFunction | Spacecraft/Actuators/Reaction Jets/Dot Product4 (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\fixedandfloat\sfix_dot.mexw32 (open) | Simulink (7.1) |
| SFunction | Spacecraft/Actuators/Reaction Jets/Dot Product5 (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\fixedandfloat\sfix_dot.mexw32 (open) | Simulink (7.1) |
| SFunction | Spacecraft/Actuators/Reaction Jets/Dot Product6 (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\fixedandfloat\sfix_dot.mexw32 (open) | Simulink (7.1) |
| SFunction | Spacecraft/Actuators/Reaction Jets/Dot Product7 (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\fixedandfloat\sfix_dot.mexw32 (open) | Simulink (7.1) |
| SFunction | Spacecraft/Actuators/Reaction Jets/Dot Product8 (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\fixedandfloat\sfix_dot.mexw32 (open) | Simulink (7.1) |
| SFunction | Spacecraft/Actuators/Reaction Jets/Dot Product9 (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\fixedandfloat\sfix_dot.mexw32 (open) | Simulink (7.1) |
| SFunction | Spacecraft/Equations of Motion/Quaternion and Spacecraft Rotational Dynamics/Compute Actual DCM/Get |q|^2 (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\fixedandfloat\sfix_dot.mexw32 (open) | Simulink (7.1) |
| SFunction | Spacecraft/Equations of Motion/Quaternion and Spacecraft Rotational Dynamics/Magnitude of q/q dot q (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\fixedandfloat\sfix_dot.mexw32 (open) | Simulink (7.1) |
| SFunction | Spacecraft/Equations of Motion/Quaternion and Spacecraft Rotational Dynamics/q * omega1 (dot product) (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\fixedandfloat\sfix_dot.mexw32 (open) | Simulink (7.1) |
| SFunction | Spacecraft/Equations of Motion/Translation/Compute |r|^2/Dot Product (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\fixedandfloat\sfix_dot.mexw32 (open) | Simulink (7.1) |
| SFunction | Spacecraft/GN&C Subsystem/Cross Product Steering/Quaternion Cross Product Matrix Q/Minus q1 (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\fixedandfloat\sfix_abs.mexw32 (open) | Simulink (7.1) |
| SFunction | Spacecraft/GN&C Subsystem/Cross Product Steering/Quaternion Cross Product Matrix Q/Minus q2 (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\fixedandfloat\sfix_abs.mexw32 (open) | Simulink (7.1) |
| SFunction | Spacecraft/GN&C Subsystem/Cross Product Steering/Quaternion Cross Product Matrix Q/Minus q3 (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\fixedandfloat\sfix_abs.mexw32 (open) | Simulink (7.1) |
| SFunction | Spacecraft/GN&C Subsystem/Guidance Commands/Compute Desired Quaternion and Accel for Thrust/Compute Command Accel Mag./Dot Product (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\fixedandfloat\sfix_dot.mexw32 (open) | Simulink (7.1) |
| SFunction | Spacecraft/GN&C Subsystem/Guidance Commands/Landing Guidance/Compute |r|^2/Dot Product (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\fixedandfloat\sfix_dot.mexw32 (open) | Simulink (7.1) |
| SFunction | Spacecraft/GN&C Subsystem/Guidance Commands/Orbit Insertion Guidance/Compute |r|^2/Dot Product (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\fixedandfloat\sfix_dot.mexw32 (open) | Simulink (7.1) |
| SFunction | Spacecraft/GN&C Subsystem/Guidance Commands/Rendezvous Guidance/Compute |r|^2/Dot Product (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\fixedandfloat\sfix_dot.mexw32 (open) | Simulink (7.1) |
| SFunction | Spacecraft/GN&C Subsystem/Guidance Commands/Trans Earth Guidance/Compute |r|^2/Dot Product (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\fixedandfloat\sfix_dot.mexw32 (open) | Simulink (7.1) |
| SFunction | Spacecraft/GN&C Subsystem/Inertial System (Strapdown)/Quaternion Estimate from Measured Rates/q_1 . omega (dot product) (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\fixedandfloat\sfix_dot.mexw32 (open) | Simulink (7.1) |
| SFunction | Spacecraft/GN&C Subsystem/Cross Product Steering/Quaternion Cross Product Matrix Q/Minus q1 (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\fixedandfloat\tlc_c\sfix_abs.tlc (open) | Simulink (7.1) |
| SFunction | Spacecraft/GN&C Subsystem/Cross Product Steering/Quaternion Cross Product Matrix Q/Minus q2 (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\fixedandfloat\tlc_c\sfix_abs.tlc (open) | Simulink (7.1) |
| SFunction | Spacecraft/GN&C Subsystem/Cross Product Steering/Quaternion Cross Product Matrix Q/Minus q3 (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\fixedandfloat\tlc_c\sfix_abs.tlc (open) | Simulink (7.1) |
| SFunction | Spacecraft/Actuators/Reaction Jets/Dot Product (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\fixedandfloat\tlc_c\sfix_dot.tlc (open) | Simulink (7.1) |
| SFunction | Spacecraft/Actuators/Reaction Jets/Dot Product1 (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\fixedandfloat\tlc_c\sfix_dot.tlc (open) | Simulink (7.1) |
| SFunction | Spacecraft/Actuators/Reaction Jets/Dot Product10 (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\fixedandfloat\tlc_c\sfix_dot.tlc (open) | Simulink (7.1) |
| SFunction | Spacecraft/Actuators/Reaction Jets/Dot Product11 (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\fixedandfloat\tlc_c\sfix_dot.tlc (open) | Simulink (7.1) |
| SFunction | Spacecraft/Actuators/Reaction Jets/Dot Product2 (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\fixedandfloat\tlc_c\sfix_dot.tlc (open) | Simulink (7.1) |
| SFunction | Spacecraft/Actuators/Reaction Jets/Dot Product3 (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\fixedandfloat\tlc_c\sfix_dot.tlc (open) | Simulink (7.1) |
| SFunction | Spacecraft/Actuators/Reaction Jets/Dot Product4 (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\fixedandfloat\tlc_c\sfix_dot.tlc (open) | Simulink (7.1) |
| SFunction | Spacecraft/Actuators/Reaction Jets/Dot Product5 (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\fixedandfloat\tlc_c\sfix_dot.tlc (open) | Simulink (7.1) |
| SFunction | Spacecraft/Actuators/Reaction Jets/Dot Product6 (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\fixedandfloat\tlc_c\sfix_dot.tlc (open) | Simulink (7.1) |
| SFunction | Spacecraft/Actuators/Reaction Jets/Dot Product7 (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\fixedandfloat\tlc_c\sfix_dot.tlc (open) | Simulink (7.1) |
| SFunction | Spacecraft/Actuators/Reaction Jets/Dot Product8 (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\fixedandfloat\tlc_c\sfix_dot.tlc (open) | Simulink (7.1) |
| SFunction | Spacecraft/Actuators/Reaction Jets/Dot Product9 (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\fixedandfloat\tlc_c\sfix_dot.tlc (open) | Simulink (7.1) |
| SFunction | Spacecraft/Equations of Motion/Quaternion and Spacecraft Rotational Dynamics/Compute Actual DCM/Get |q|^2 (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\fixedandfloat\tlc_c\sfix_dot.tlc (open) | Simulink (7.1) |
| SFunction | Spacecraft/Equations of Motion/Quaternion and Spacecraft Rotational Dynamics/Magnitude of q/q dot q (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\fixedandfloat\tlc_c\sfix_dot.tlc (open) | Simulink (7.1) |
| SFunction | Spacecraft/Equations of Motion/Quaternion and Spacecraft Rotational Dynamics/q * omega1 (dot product) (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\fixedandfloat\tlc_c\sfix_dot.tlc (open) | Simulink (7.1) |
| SFunction | Spacecraft/Equations of Motion/Translation/Compute |r|^2/Dot Product (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\fixedandfloat\tlc_c\sfix_dot.tlc (open) | Simulink (7.1) |
| SFunction | Spacecraft/GN&C Subsystem/Guidance Commands/Compute Desired Quaternion and Accel for Thrust/Compute Command Accel Mag./Dot Product (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\fixedandfloat\tlc_c\sfix_dot.tlc (open) | Simulink (7.1) |
| SFunction | Spacecraft/GN&C Subsystem/Guidance Commands/Landing Guidance/Compute |r|^2/Dot Product (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\fixedandfloat\tlc_c\sfix_dot.tlc (open) | Simulink (7.1) |
| SFunction | Spacecraft/GN&C Subsystem/Guidance Commands/Orbit Insertion Guidance/Compute |r|^2/Dot Product (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\fixedandfloat\tlc_c\sfix_dot.tlc (open) | Simulink (7.1) |
| SFunction | Spacecraft/GN&C Subsystem/Guidance Commands/Rendezvous Guidance/Compute |r|^2/Dot Product (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\fixedandfloat\tlc_c\sfix_dot.tlc (open) | Simulink (7.1) |
| SFunction | Spacecraft/GN&C Subsystem/Guidance Commands/Trans Earth Guidance/Compute |r|^2/Dot Product (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\fixedandfloat\tlc_c\sfix_dot.tlc (open) | Simulink (7.1) |
| SFunction | Spacecraft/GN&C Subsystem/Inertial System (Strapdown)/Quaternion Estimate from Measured Rates/q_1 . omega (dot product) (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\fixedandfloat\tlc_c\sfix_dot.tlc (open) | Simulink (7.1) |
| BlockCallback,MaskInitialization | Spacecraft/GN&C Subsystem/Inertial System (Strapdown)/Quaternion Estimate from Measured Rates/Magnitude of q (show) | C:\Program Files\MATLAB\R2008a\toolbox\aeroblks\aeroblks\aeroicon.m (open) | Aerospace Blockset (3.1) |
| BlockCallback,MaskInitialization | Spacecraft/GN&C Subsystem/Inertial System (Strapdown)/Quaternion Estimate from Measured Rates/q_1 cross omeqa (show) | C:\Program Files\MATLAB\R2008a\toolbox\aeroblks\aeroblks\aeroicon.m (open) | Aerospace Blockset (3.1) |
| BlockCallback,MaskInitialization | Spacecraft/Strap Down Sensors (Body Coords)/Strap Down Accelerometers (show) | C:\Program Files\MATLAB\R2008a\toolbox\aeroblks\aeroblks\aeroicon.m (open) | Aerospace Blockset (3.1) |
| BlockCallback,MaskInitialization | Spacecraft/Strap Down Sensors (Body Coords)/Strap Down Accelerometers/w x (w x d)/w x (w x d) (show) | C:\Program Files\MATLAB\R2008a\toolbox\aeroblks\aeroblks\aeroicon.m (open) | Aerospace Blockset (3.1) |
| BlockCallback,MaskInitialization | Spacecraft/Strap Down Sensors (Body Coords)/Strap Down Accelerometers/w x (w x d)/w x d (show) | C:\Program Files\MATLAB\R2008a\toolbox\aeroblks\aeroblks\aeroicon.m (open) | Aerospace Blockset (3.1) |
| BlockCallback,MaskInitialization | Spacecraft/Strap Down Sensors (Body Coords)/Strap Down Accelerometers/wdot x d (show) | C:\Program Files\MATLAB\R2008a\toolbox\aeroblks\aeroblks\aeroicon.m (open) | Aerospace Blockset (3.1) |
| BlockCallback,MaskInitialization | Spacecraft/Strap Down Sensors (Body Coords)/Strap Down Rate Gyros (show) | C:\Program Files\MATLAB\R2008a\toolbox\aeroblks\aeroblks\aeroicon.m (open) | Aerospace Blockset (3.1) |
| BlockCallback,MaskDisplay | Spacecraft/Actuators (show) | C:\Program Files\MATLAB\R2008a\toolbox\matlab\imagesci\imread.m (open) | MATLAB (7.6) |
| BlockCallback,MaskDisplay | Spacecraft/Equations of Motion (show) | C:\Program Files\MATLAB\R2008a\toolbox\matlab\imagesci\imread.m (open) | MATLAB (7.6) |
| BlockCallback,MaskDisplay | Spacecraft/GN&C Subsystem (show) | C:\Program Files\MATLAB\R2008a\toolbox\matlab\imagesci\imread.m (open) | MATLAB (7.6) |
| BlockCallback,MaskDisplay | Spacecraft/Strap Down Sensors (Body Coords) (show) | C:\Program Files\MATLAB\R2008a\toolbox\matlab\imagesci\imread.m (open) | MATLAB (7.6) |
| BlockCallback,MaskInitialization | Spacecraft/GN&C Subsystem/Guidance Commands/Landing Guidance/v(1) < 1? (show) | C:\Program Files\MATLAB\R2008a\toolbox\matlab\strfun\num2str.m (open) | MATLAB (7.6) |
| BlockCallback,MaskInitialization | Spacecraft/GN&C Subsystem/Guidance Commands/Orbit Insertion Guidance/v(1) < 0.5? (show) | C:\Program Files\MATLAB\R2008a\toolbox\matlab\strfun\num2str.m (open) | MATLAB (7.6) |
| BlockCallback,MaskInitialization | Spacecraft/GN&C Subsystem/Guidance Commands/Rendezvous Guidance/v(1) < 0.5? (show) | C:\Program Files\MATLAB\R2008a\toolbox\matlab\strfun\num2str.m (open) | MATLAB (7.6) |
| BlockCallback,MaskInitialization | Spacecraft/GN&C Subsystem/Guidance Commands/Trans Earth Guidance/v(1) < 0.5? (show) | C:\Program Files\MATLAB\R2008a\toolbox\matlab\strfun\num2str.m (open) | MATLAB (7.6) |
| BlockCallback,MaskInitialization | Spacecraft/GN&C Subsystem/Guidance Commands/Landing Guidance/v(1) < 1? (show) | C:\Program Files\MATLAB\R2008a\toolbox\matlab\strfun\str2num.m (open) | MATLAB (7.6) |
| BlockCallback,MaskInitialization | Spacecraft/GN&C Subsystem/Guidance Commands/Orbit Insertion Guidance/v(1) < 0.5? (show) | C:\Program Files\MATLAB\R2008a\toolbox\matlab\strfun\str2num.m (open) | MATLAB (7.6) |
| BlockCallback,MaskInitialization | Spacecraft/GN&C Subsystem/Guidance Commands/Rendezvous Guidance/v(1) < 0.5? (show) | C:\Program Files\MATLAB\R2008a\toolbox\matlab\strfun\str2num.m (open) | MATLAB (7.6) |
| BlockCallback,MaskInitialization | Spacecraft/GN&C Subsystem/Guidance Commands/Trans Earth Guidance/v(1) < 0.5? (show) | C:\Program Files\MATLAB\R2008a\toolbox\matlab\strfun\str2num.m (open) | MATLAB (7.6) |
| BlockCallback,MaskInitialization | Spacecraft/Equations of Motion/Translation/Altitude Probe/Compare To Zero (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\simulink\gcb.m (open) | Simulink (7.1) |
| BlockCallback,MaskInitialization | Spacecraft/GN&C Subsystem/Guidance Commands/Landing Guidance/v(1) < 1? (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\simulink\gcb.m (open) | Simulink (7.1) |
| BlockCallback,MaskInitialization | Spacecraft/GN&C Subsystem/Guidance Commands/Orbit Insertion Guidance/v(1) < 0.5? (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\simulink\gcb.m (open) | Simulink (7.1) |
| BlockCallback,MaskInitialization | Spacecraft/GN&C Subsystem/Guidance Commands/Rendezvous Guidance/v(1) < 0.5? (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\simulink\gcb.m (open) | Simulink (7.1) |
| BlockCallback,MaskInitialization | Spacecraft/GN&C Subsystem/Guidance Commands/Trans Earth Guidance/v(1) < 0.5? (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\simulink\gcb.m (open) | Simulink (7.1) |
| BlockCallback,MaskInitialization | Spacecraft/Strap Down Sensors (Body Coords)/Strap Down Accelerometers (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\simulink\gcb.m (open) | Simulink (7.1) |
| BlockCallback,MaskInitialization | Spacecraft/Strap Down Sensors (Body Coords)/Strap Down Accelerometers/Random bias (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\simulink\gcb.m (open) | Simulink (7.1) |
| BlockCallback,MaskInitialization | Spacecraft/Strap Down Sensors (Body Coords)/Strap Down Rate Gyros (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\simulink\gcb.m (open) | Simulink (7.1) |
| BlockCallback,MaskInitialization | Spacecraft/Strap Down Sensors (Body Coords)/Strap Down Rate Gyros/Random bias (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\simulink\gcb.m (open) | Simulink (7.1) |
| BlockCallback,MaskDisplay | Spacecraft/Actuators (show) | C:\work\Simulink2007Tour\LunarEx\CEV\SourceFiles\actuator.JPG (open) | (not in a toolbox) |
| BlockCallback,MaskDisplay | Spacecraft/GN&C Subsystem (show) | C:\work\Simulink2007Tour\LunarEx\CEV\SourceFiles\GNC.JPG (open) | (not in a toolbox) |
| BlockCallback,MaskDisplay | Spacecraft/Equations of Motion (show) | C:\work\Simulink2007Tour\LunarEx\CEV\SourceFiles\LSAM_Descent.bmp (open) | (not in a toolbox) |
| BlockCallback,MaskDisplay | Spacecraft/Strap Down Sensors (Body Coords) (show) | C:\work\Simulink2007Tour\LunarEx\CEV\SourceFiles\sensor.JPG (open) | (not in a toolbox) |
| LibraryLink | Spacecraft_Library/ Transformation Quaternion2DCM/Quaternions to Direction Cosine Matrix (show) | C:\Program Files\MATLAB\R2008a\toolbox\aeroblks\aeroblks\aerolibtransform2.mdl (open) | Aerospace Blockset (3.1) |
| LibraryLink | Spacecraft_Library/Equations of Motion for Quaternion and Spacecraft Rotational Dynamics/3x3 cross product1 (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\simdemos\aerospace\aerospace.mdl (open) | Simulink (7.1) |
| LibraryLink | Spacecraft_Library/Equations of Motion for Quaternion and Spacecraft Rotational Dynamics/q cross omega1 (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\simdemos\aerospace\aerospace.mdl (open) | Simulink (7.1) |
| LibraryLink | Spacecraft_Library/Navigation Estimate Quaternions from Measured Rates/Magnitude of q (show) | C:\Program Files\MATLAB\R2008a\toolbox\aeroblks\aeroblks\aerolibutil.mdl (open) | Aerospace Blockset (3.1) |
| LibraryLink | Spacecraft_Library/Navigation Estimate Quaternions from Measured Rates/q_1 cross omeqa (show) | C:\Program Files\MATLAB\R2008a\toolbox\aeroblks\aeroblks\aerolibutil.mdl (open) | Aerospace Blockset (3.1) |
| LibraryLink | Spacecraft_Library/Transformation Quaternion2Euler (x-Yaw, y-Pitch, z-Roll)/Quaternions to Rotation Angles (show) | C:\Program Files\MATLAB\R2008a\toolbox\aeroblks\aeroblks\aerolibtransform2.mdl (open) | Aerospace Blockset (3.1) |
| Stateflow | Spacecraft_Library/RCS Control Law/Switch Curve Decision Logic (show) | C:\Program Files\MATLAB\R2008a\toolbox\stateflow\stateflow\sf_sfun.mexw32 (open) | Stateflow (7.1) |
| SFunction | Spacecraft_Library/Equations of Motion for Quaternion and Spacecraft Rotational Dynamics/Compute Actual DCM/Get |q|^2 (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\fixedandfloat\sfix_dot.mexw32 (open) | Simulink (7.1) |
| SFunction | Spacecraft_Library/Equations of Motion for Quaternion and Spacecraft Rotational Dynamics/Magnitude of q/q dot q (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\fixedandfloat\sfix_dot.mexw32 (open) | Simulink (7.1) |
| SFunction | Spacecraft_Library/Equations of Motion for Quaternion and Spacecraft Rotational Dynamics/q * omega1 (dot product) (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\fixedandfloat\sfix_dot.mexw32 (open) | Simulink (7.1) |
| SFunction | Spacecraft_Library/Navigation Estimate Quaternions from Measured Rates/q . omega (dot product) (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\fixedandfloat\sfix_dot.mexw32 (open) | Simulink (7.1) |
| SFunction | Spacecraft_Library/Equations of Motion for Quaternion and Spacecraft Rotational Dynamics/Compute Actual DCM/Get |q|^2 (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\fixedandfloat\tlc_c\sfix_dot.tlc (open) | Simulink (7.1) |
| SFunction | Spacecraft_Library/Equations of Motion for Quaternion and Spacecraft Rotational Dynamics/Magnitude of q/q dot q (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\fixedandfloat\tlc_c\sfix_dot.tlc (open) | Simulink (7.1) |
| SFunction | Spacecraft_Library/Equations of Motion for Quaternion and Spacecraft Rotational Dynamics/q * omega1 (dot product) (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\fixedandfloat\tlc_c\sfix_dot.tlc (open) | Simulink (7.1) |
| SFunction | Spacecraft_Library/Navigation Estimate Quaternions from Measured Rates/q . omega (dot product) (show) | C:\Program Files\MATLAB\R2008a\toolbox\simulink\fixedandfloat\tlc_c\sfix_dot.tlc (open) | Simulink (7.1) |
| BlockCallback,MaskInitialization | Spacecraft_Library/ Transformation Quaternion2DCM/Quaternions to Direction Cosine Matrix (show) | C:\Program Files\MATLAB\R2008a\toolbox\aeroblks\aeroblks\aeroicon.m (open) | Aerospace Blockset (3.1) |
| BlockCallback,MaskInitialization | Spacecraft_Library/Navigation Estimate Quaternions from Measured Rates/Magnitude of q (show) | C:\Program Files\MATLAB\R2008a\toolbox\aeroblks\aeroblks\aeroicon.m (open) | Aerospace Blockset (3.1) |
| BlockCallback,MaskInitialization | Spacecraft_Library/Navigation Estimate Quaternions from Measured Rates/q_1 cross omeqa (show) | C:\Program Files\MATLAB\R2008a\toolbox\aeroblks\aeroblks\aeroicon.m (open) | Aerospace Blockset (3.1) |
| BlockCallback,MaskInitialization | Spacecraft_Library/Transformation Quaternion2Euler (x-Yaw, y-Pitch, z-Roll)/Quaternions to Rotation Angles (show) | C:\Program Files\MATLAB\R2008a\toolbox\aeroblks\aeroblks\aeroicon.m (open) | Aerospace Blockset (3.1) |
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