Delta D25886 User Manual Page 248
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- Table of contents
- TROUBLESHOOTING
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4. Motion Control Instructions
DVP-MC operating manual 4-207
A_Pos
The coordinate position of terminal point of the
added axis
REAL Constant, D
B_Pos
The coordinate position of terminal point of the
added axis
REAL Constant, D
C_Pos
The coordinate position of terminal point of the
added axis
REAL Constant, D
P_Pos
The coordinate position of terminal point of the
added axis
REAL Constant, D
Q_Pos
The coordinate position of terminal point of the
added axis
REAL Constant, D
R_Value
The radius of the circular arc. Positive number is
minor arc and negative number is major arc.
REAL Constant, D
T_Value The quantity of the full circle UINT Constant, D
Velocity The feed speed of the circular arc REAL Constant, D
Acceleration Acceleration REAL Constant, D
Deceleration Deceleration REAL Constant, D
GroupID
The number of the coordinate motion instruction
group, range: 0~7.
When the instruction is executed, the group ID
should be consistent with that of DNC_Group.
UINT Constant, D
Done
When the execution of the instruction is finished,
“Done” is on; when “Execute”
turns off, “Done” is reset.
BOOL M,Q
Error
If any error is detected, "Error" turns on; when
"Execute" turns off, "Error" is reset.
BOOL M,Q
ErrorID Error code. Please refer to section 5.3. UINT D
Note:
1. The function of the instruction DNC_CW(R) (G2) and DNC_CCW(R) (G3) is same as that of G2 and
G3 in G codes and the input parameters X_Pos~Deceleration in the instruction and the parameters
of X_, Y_, Z_, A_, B_, C_, P_, Q_, R_,T_, F_,E_,E_ in G2 and G3 have same explanation. For more
details on G2 and G3, please refer to section 4.8.3.5.
2. The state of axis related with the instruction is Standstill. After “DNC_Group” is executed, the
instruction just can be executed and its GroupID must be same as that of DNC_Group.
3. The instruction can be switched to absolute mode via DNC_Absolute (90). In absolute mode, the
terminal position of each axis is based on 0 unit.
4. The instruction can be switched to relative mode via DNC_Relative (91). In relative mode, the
terminal position of each axis is calculated as incremental value beginning from current position.
5. It is absolute mode for the instruction by default. Therefore, it is absolute mode for DNC_CW (R) (G2)
and DNC_CCW(R) (G3) if DNC_Absolute (90) and DNC_Relative (91) have not been executed.
- DVP-MC Bus-Type 1
- Multi-Axis Motion Controller 1
- Operating Manual 1
- Content 2
- Overview of DVP10MC11T 7
- 2. System Function 10
- 3. System Installation 34
- 4.1. Instruction Table 42
- 4.2. Axis Status 46
- 4.3. Instruction Usage 47
- Instruction format 47
- Data type list 48
- 4.4.1. MC_MoveAbsolute 49
- Program Example (1) 52
- Program Example (2) 53
- 4.4.2. MC_MoveRelative 55
- 4.4.3. MC_MoveAdditive 59
- 4.4.4. MC_MoveSuperImposed 63
- 4.4.5. MC_MoveVelocity 68
- 4.4.6. MC_Stop 71
- 4.4.7. MC_PassiveHome 74
- Example 75
- 4.4.8. MC_Power 77
- 4.4.9. MC_Reset 78
- Exmaple: 79
- 4.4.10. MC_ReadStatus 80
- 4.4.12. MC_ReadAxisError 82
- 4.4.13. DMC_ReadParameter 83
- 4.4.14. DMC_WriteParameter 84
- 4.4.15. DMC_SetTorque 85
- Program Example 86
- 4.5.1. MC_CamTableSelect 87
- 4.5.2. MC_CamIn 88
- = 0, slave position is 101
- 0, slave offset = 0 102
- Master Positio 102
- offset = 40, slave position 103
- Electronic cam example: 104
- Position 105
- 4.5.3. MC_CamOut 107
- Program Example: 108
- 4.5.4. DMC_CamSet 110
- Acceleration 112
- 4.5.5. MC_GearIn 114
- . UINT D 115
- 4.5.7. MC_Phasing 118
- Sequence Diagram 120
- 4.5.8. DMC_CapturePosition 121
- 4.5.9. DMC_VirtualAxis 127
- 4.5.10. DMC_ExternalMaster 129
- 4.6. Logical Instruction 131
- 4.6.3. ADD_R 132
- 4.6.4. SUB 132
- 4.6.5. SUB_DI 133
- 4.6.6. SUB_R 133
- 4.6.7. MUL 134
- 4.6.8. MUL_DI 134
- 4.6.9. MUL_R 135
- 4.6.10. DIV 135
- 4.6.11. DIV_DI 136
- 4.6.12. DIV_R 136
- 4.6.13. AND 137
- 4.6.14. OR 137
- 4.6.15. XOR 138
- 4.6.16. NOT 138
- 4.6.17. CTU 139
- Program example: 140
- 4.6.18. CTD 141
- 4.6.19. CTUD 143
- 4.6.20. TON_s 145
- 4.6.21. TOF_s 147
- 4.6.22. TONR_s 149
- 4.6.23. TON_ms 151
- 4.6.24. TOF_ms 152
- 4.6.25. TONR_ms 153
- 4.6.26. CMP 154
- 4.6.27. CMP_DI 155
- 4.6.28. CMP_R 156
- 4.6.30. MOV_DI 158
- 4.6.31. MOV_R 158
- 4.6.34. MOVF_R 161
- Program example : 162
- 4.6.36. MOV_BW 163
- 4.6.38. ZCP 165
- 4.6.39. ZCP_DI 166
- 4.6.40. ZCP_R 167
- 168
- 4.6.43. OUT 169
- 4.6.44. R_Trig 169
- 4.6.46. ZRSTM 172
- 4.6.47. ZRSTD 173
- 4.6.48. SQRT_R 174
- 4.6.49. MOD 174
- 4.6.50. MOD_DI 175
- 4.6.51. MOD_R 175
- 4.6.52. Real_To_Int 176
- 4.6.53. Real_To_DInt 176
- 4.6.54. Int_To_Real 177
- 4.6.55. DInt_To_Real 177
- Example 1: 178
- Example 2: 179
- Example 3: 179
- 4.6.58. Offset _R 182
- 4.7. Application Instruction 183
- 4.7.2. Rotary Cut Parameters 184
- Short material cutting 185
- Equal length cutting 185
- The entry curve 187
- The end curve 188
- 4.7.5.1 189
- 4.7.5.2. APF_RotaryCut_In 191
- 4.7.5.3. APF_RotaryCut_Out 192
- Explanation of areas 197
- Steps for flying shear 197
- Function feature 197
- Shear axis 198
- Sync area 203
- 4.8.1. G Code Input Format 206
- Center of a circle 222
- Start point 222
- Terminal point 222
- （）200,200 223
- Start point Start point 226
- Instruction example 1: 232
- Instruction example 2: 232
- Instruction example: 232
- 4.8.4. DMC_NC 233
- Program example 1: 235
- Program example 2: 236
- ¾ Program: 237
- ¾ Steps: 237
- 5.Troubleshooting 258
- 5. Troubleshooting 259
- Appendix A 264
- Appendix B 287
- Appendix C 301
- Appendix D 333
- Appendix E 338
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