MC33030 ONSEMI | Alldatasheet
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/C0077/C0067/C0051/C0051/C0048/C0051/C0048 SEMICONDUCTOR TECHNICAL DATA DC SERVO MOTOR CONTROLLER/DRIVER Order this document by MC33030/D 11 6 (Top View) Reference Input Reference Input Filter Error Amp Output Filter/Feedback Input Gnd Error Amp Output Error Amp Inverting Input Error Amp Non– Inverting Input Over–Current Delay Gnd Error Amp Input Filter PIN CONNECTIONS Device Operating Temperature Range Package
ORDERING INFORMATION
TA = –40° to +85°C SOP–16L DIP–16 P SUFFIX PLASTIC PACKAGE CASE 648C (DIP–16) DW SUFFIX PLASTIC PACKAGE CASE 751G (SOP–16L) Driver Output B VCC Driver Output A Over–Current Reference Pins 4, 5, 12 and 13 are electrical ground and heat sink pins for IC. 1MOTOROLA ANALOG IC DEVICE DATA /C0068/C0067 /C0083/C0101/C0114/C0118/C0111 /C0077/C0111/C0116/C0111/C0114 /C0067/C0111/C0110/C0116/C0114/C0111/C0108/C0108/C0101/C0114/C0047/C0068/C0114/C0105/C0118/C0101/C0114 The MC33030 is a monolithic DC servo motor controller providing all active functions necessary for a complete closed loop system. This device consists of an on–chip op amp and window comparator with wide input common–mode range, drive and brake logic with direction memory, Power H–Switch driver capable of 1.0 A, independently programmable over–current monitor and shutdown delay, and over–voltage monitor. This part is ideally suited for almost any servo positioning application that requires sensing of temperature, pressure, light, magnetic flux, or any other means that can be converted to a voltage. Although this device is primarily intended for servo applications, it can be used as a switchmode motor controller.
- On–Chip Error Amp for Feedback Monitoring
- Window Detector with Deadband and Self Centering Reference Input
- Drive/Brake Logic with Direction Memory
- 1.0 A Power H–Switch
- Programmable Over–Current Detector
- Programmable Over–Current Shutdown Delay
- Over–Voltage Shutdown Motor 141011 VCC R OCC DLY 1516 Power H–Switch Programmable Over– Current Detector & Latch 4, 5, 12, 13 Reference Position VCC – Direction Memory Window Detector Drive/ Brake Logic Over– Voltage Monitor Error Amp 9Feedback Position VCC Representative Block Diagram This device contains 119 active transistors. Motorola, Inc. 1996 Rev 2
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Power Supply Voltage VCC 36 V Input Voltage Range O A C t C t Li it VIR –0.3 to VCC Vpg g Op Amp, Comparator, Current Limit ( P i 12367891 5 ) IR CC Input Differential Voltage Range Op Amp Comparator (Pins1236789 ) VIDR –0.3 to VCC V Op Amp, Comparator (Pins 1, 2, 3, 6, 7, 8, 9) Delay Pin Sink Current (Pin 16) IDLY(sink) 20 mA Output Source Current (Op Amp) Isource 10 mA Drive Output Voltage Range (Note 1) VDRV –0.3 to (VCC + VF) V Drive Output Source Current (Note 2) IDRV(source) 1.0 A Drive Output Sink Current (Note 2) IDRV(sink) 1.0 A Brake Diode Forward Current (Note 2) IF 1.0 A Power Dissipation and Thermal Characteristics °C/W Ch aracteristics P Suffix, Dual In Line Case 648CSu , ua e Case 6 8C Thermal Resistance, Junction–to–Air Thermal Resistance Junction–to–Case R θJA R θJC 15Thermal R esistance, Junction–to–C ase R θJC 15 DW Suffix, Dual In Line Case 751G Thermal Resistance Junction to Air R θJA 94Thermal Resistance, Junction–to–Air Thermal Resistance, Junction–to–Case R θJA R θJC 18Thermal Resistance, Junction to Case R θJC 18 Operating Junction Temperature TJ +150 °C Operating Ambient Temperature Range TA –40 to +85 °C Storage Temperature Range Tstg –65 to +150 °C NOTES : 1. The upper voltage level is clamped by the forward drop, VF, of the brake diode. 2. These values are for continuous DC current. Maximum package power dissipation limits must be observed. ELECTRICAL CHARACTERISTICS (VCC = 14 V, TA = 25°C, unless otherwise noted.) Characteristic Symbol Min Typ Max Unit ERROR AMP Input Offset Voltage (– 40°C /C0112 TA /C0112 85°C) V 7 0 V R 100 k VIO – 1.5 10 mV VPin 6 = 7.0 V, RL = 100 k Input Offset Current (VPin 6 = 1.0 V, RL = 100 k) IIO – 0.7 – nA Input Bias Current (VPin 6 = 7.0 V, RL = 100 k) IIB – 7.0 – nAInput Bias Current (VPin 6 = 7.0 V, R L = 100 k) IIB – 7.0 – nA Input Common–Mode Voltage Range ΔV 20 mV R 100 k VICR – 0 to (VCC – 1.2) – V ΔVIO = 20 mV, RL = 100 k Slew Rate, Open Loop (VID = 0.5 V, CL = 15 pF) SR – 0.40 – V/µs Unity–Gain Crossover Frequency fc – 550 – kHz Unity–Gain Phase Margin φm – 63 – deg. Common–Mode Rejection Ratio (VPin 6 = 7.0 V, RL = 100 k) CMRR 50 82 – dB Power Supply Rejection Ratio V 90t o1 6V V 70V R 1 0 0k PSRR – 89 – dB VCC = 9.0 to 16 V, VPin 6 = 7.0 V, RL = 100 k Output Source Current (VPin 6 = 12 V) IO + – 1.8 – mA Output Sink Current (VPin 6 = 1.0 V) IO – – 250 – µA Output Voltage Swing (RL = 17 k to Ground) VOH VOL 12.5 13.1 0.02 V V NOTES : 3. The upper or lower hysteresis will be lost when operating the Input, Pin 3, close to the respective rail. Refer to Figure 4. 4. Low duty cycle pulse techniques are used during test to maintain junction temperature as close to ambient temperature as possible.
3MOTOROLA ANALOG IC DEVICE DATA ELECTRICAL CHARACTERISTICS (continued) (VCC = 14 V, TA = 25°C, unless otherwise noted.) Characteristic Symbol Min Typ Max Unit WINDOW DETECTOR Input Hysteresis Voltage (V1 – V4, V2 – V3, Figure 18) VH 25 35 45 mV Input Dead Zone Range (V2 – V4, Figure 18) VIDZ 166 210 254 mV Input OffsetVoltage ([V2 – VPin 2] – [VPin 2 – V4] Figure 18) VIO – 25 – mV Input Functional Common–Mode Range (Note 3) UT h h l d V (V 1 05) Vpg ( ) Upper Threshold LT h h l d VIH V – (VCC – 1.05) 02 4 Lower Threshold VIL – 0.24 – Reference Input Self Centering Voltage Pins 1 and 2 Open VRSC – (1/2 VCC ) – V Pins 1 and 2 Open Window Detector Propagation Delay C t I t Pi 3 t D i O t t tp(IN/DRV) – 2.0 – µspg y Comparator Input, Pin 3, to Drive Outputs V 0 5 V R 390 Ω p(IN/DRV) µ VID = 0.5 V, RL(DRV) = 390 Ω OVER–CURRENT MONITOR Over–Current Reference Resistor Voltage (Pin 15) R OC 3.9 4.3 4.7 V Delay Pin Source Current V 0 V R 27 k I 0 mA IDLY(source) – 5.5 6.9 µA VDLY = 0 V, ROC = 27 k, IDRV = 0 mA Delay Pin Sink Current (ROC = 27 k, IDRV = 0 mA) V5 0 V IDLY(sink) mAy( OC DRV ) VDLY = 5.0 V V8 3 V DLY(sink) – 0.1 VDLY = 8.3 V V1 4 V – 0.7 16 5 VDLY = 14 V – 16.5 – Delay Pin Voltage, Low State (IDLY = 0 mA) VOL(DLY) – 0.3 0.4 V Over–Current Shutdown Threshold V1 4 V Vth(OC) 68 75 82 V VCC = 14 V V8 0 V th(OC) 6.8 7.5 8.2 65VCC = 8.0 V 5.5 6.0 6.5 Over–Current Shutdown Propagation Delay Delay Capacitor Input, Pin 16, to Drive Outputs, VID = 0.5 V tp(DLY/DRV) – 1.8 – µs POWER H–SWITCH Drive–Output Saturation (– 40°C /C0112 TA /C0112+ 85°C, Note 4) Hi h St t (I 100 A) V (V 2) (V 0 85) Vp( A ) High–State (I source = 100 mA) L St t (I 100 A) VOH(DRV) V (VCC – 2) (VCC – 0.85) 01 2 10Low–State (I sink = 100 mA) VOL(DRV) – 0.12 1.0 Drive–Output Voltage Switching Time (CL = 15 pF) Ri Ti t 200 nspg g ( L p) Rise Time Fl l T i tr t – 200 200 Fall Time tf – 200 – Brake Diode Forward Voltage Drop (IF = 200 mA, Note 4) VF – 1.04 2.5 V TOTAL DEVICE Standby Supply Current ICC – 14 25 mA Over–Voltage Shutdown Threshold (4 0°C /C0112T /C011285°C) Vth(OV) 16.5 18 20.5 V (– 40°C /C0112 TA /C0112 + 85°C) Over–Voltage Shutdown Hysteresis (Device “off” to “on”) VH(OV) 0.3 0.6 1.0 V Operating Voltage Lower Threshold (4 0°C /C0112T /C011285°C) VCC – 7.5 8.0 V (– 40°C /C0112 TA /C0112 + 85°C) NOTES: 3. The upper or lower hysteresis will be lost when operating the Input, Pin 3, close to the respective rail. Refer to Figure 4. 4. Low duty cycle pulse techniques are used during test to maintain junction temperature as close to ambient temperature as possible.
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Figure 1. Error Amp Input Common–Mode Figure 2. Error Amp Output Saturation
0.1 Gnd
Figure 3. Open Loop Voltage Gain and Figure 4. Window Detector Reference–Input Figure 5. Window Detector Feedback–Input Figure 6. Output Driver Saturation
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Figure 13. Normalized Over–Voltage Shutdown Figure 14. Normalized Over–Voltage Shutdown Figure 15. P Suffix (DIP–16) Thermal Figure 16. DW Suffix (SOP–16L) Thermal
7MOTOROLA ANALOG IC DEVICE DATA OPERATING DESCRIPTION The MC33030 was designed to drive fractional horsepower DC motors and sense actuator position by voltage feedback. A typical servo application and representative internal block diagram are shown in Figure 17. The system operates by setting a voltage on the reference input of the Window Dectector (Pin 1) which appears on (Pin 2). A DC motor then drives a position sensor, usually a potentiometer driven by a gear box, in a corrective fashion so that a voltage proportional to position is present at Pin 3. The servo motor will continue to run until the voltage at Pin 3 falls within the dead zone, which is centered about the reference voltage. The Window Detector is composed of two comparators, A and B, each containing hysteresis. The reference input, common to both comparators, is pre–biased at 1/2 VCC for simple two position servo systems and can easily be overriden by an external voltage divider. The feedback voltage present at Pin 3 is connected to the center of two resistors that are driven by an equal magnitude current source and sink. This generates an offset voltage at the input of each comparator which is centered about Pin 3 that can float virtually from VCC to ground. The sum of the upper and lower offset voltages is defined as the window detector input dead zone range. To increase system flexibility, an on–chip Error Amp is provided. It can be used to buffer and/or gain–up the actuator position voltage which has the effect of narrowing the dead zone range. A PNP differential input stage is provided so that the input common–mode voltage range will include ground. The main design goal of the error amp output stage was to be able to drive the window detector input. It typically can source 1.8 mA and sink 250 µA. Special design considerations must be made if it is to be used for other applications. The Power H–Switch provides a direct means for motor drive and braking with a maximum source, sink, and brake current of 1.0 A continuous. Maximum package power dissipation limits must be observed. Refer to Figure 15 for thermal information. For greater drive current requirements, a method for buffering that maintains all the system features is shown in Figure 30. The Over–Current Monitor is designed to distinguish between motor start–up or locked rotor conditions that can occur when the actuator has reached its travel limit. A fraction of the Power H–Switch source current is internally fed into one of the two inverting inputs of the current comparator, while the non–inverting input is driven by a programmable current reference. This reference level is controlled by the resistance value selected for ROC , and must be greater than the required motor run–current with its mechanical load over temperature; refer to Figure 8. During an over–current condition, the comparator will turn off and allow the current source to charge the delay capacitor, CDLY. When C DLY charges to a level of 7.5 V, the set input of the over–current latch will go high, disabling the drive and brake functions of the Power H–Switch. The programmable time delay is determined by the capacitance value–selected for C DLY. tDLY /C0043 V refC DLY IDLY(source) /C0043
7.5 CDLY
5.5 µA /C00431.36 CDLY inµF This system allows the Power H–Switch to supply motor start–up current for a predetermined amount of time. If the rotor is locked, the system will time–out and shut–down. This feature eliminates the need for servo end–of–travel or limit switches. Care must be taken so as not to select too large of a capacitance value for CDLY. An over–current condition for an excessively long time–out period can cause the integrated circuit to overheat and eventually fail. Again, the maximum package power dissipation limits must be observed. The over–current latch is reset upon power–up or by readjusting VPin 2 as to cause VPin 3 to enter or pass through the dead zone. This can be achieved by requesting the motor to reverse direction. An Over–Voltage Monitor circuit provides protection for the integrated circuit and motor by disabling the Power H–Switch functions if VCC should exceed 18 V. Resumption of normal operation will commence when VCC falls below 17.4 V. A timing diagram that depicts the operation of the Drive/Brake Logic section is shown in Figure 18. The waveforms grouped in [1] show a reference voltage that was preset, appearing on Pin 2, which corresponds to the desired actuator position. The true actuator position is represented by the voltage on Pin 3. The points V1 through V4 represent the input voltage thresholds of comparators A and B that cause a change in their respective output state. They are defined as follows: V1 = Comparator B turn–off threshold V2 = Comparator A turn–on threshold V3 = Comparator A turn–off threshold V4 = Comparator B turn–on threshold V1–V4 = Comparator B input hysteresis voltage V2–V3 = Comparator A input hysteresis voltage V2–V4 = Window detector input dead zone range |(V2–VPin2) – (VPin2 – V4)| = Window detector input voltage It must be remembered that points V1 through V4 always try to follow and center about the reference voltage setting if it is within the input common–mode voltage range of Pin 3; Figures 4 and 5. Initially consider that the feedback input voltage level is somewhere on the dashed line between V2 and V4 in [1]. This is within the dead zone range as defined above and the motor will be off. Now if the reference voltage is raised so that VPin 3 is less than V4, comparator B will turn–on [3] enabling Q Drive, causing Drive Output A to sink and B to source motor current [8]. The actuator will move in Direction B until VPin 3 becomes greater than V1. Comparator B will turn–off, activating the brake enable [4] and Q Brake [6] causing Drive Output A to go high and B to go into a high impedance state. The inertia of the mechanical system will drive the motor as a generator creating a positive voltage on Pin 10 with respect to Pin 14. The servo system can be stopped quickly, so as not to over–shoot through the dead zone range, by braking. This is accomplished by shorting the motor/generator terminals together. Brake current will flow into the diode at Drive Output B, through the internal VCC rail, and out the emitter of the sourcing transistor at Drive Output A. The end of the solid line and beginning of the dashed for VPin 3 [1] indicates the possible resting position of the actuator after braking.
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Figure 17. Representative Block Diagram and Typical Servo Application Drive/Brake behavior for Direction A is identical to that of B. and pressure as a means to drive the feedback element. torque characteristics at low RPM.
Figure 18. Timing Diagram
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Figure 19. Solar Tracking Servo System R 3 – darkness for next sunrise. Figure 20. Magnetic Sensing Servo System Typical sensitivity with gain set at 3.9 k is 1.5 mV/gauss. Servo motor controls magnetic field about sensor. servo when end stop is reached. servo when end stop is reached. Figure 21. Infrared Latched Two Position Figure 22. Digital Two Position Servo System Figure 23. 0.25 Hz Square–Wave Figure 24. Second Order Low–Pass Active Filter
Figure 25. Notch Filter Figure 26. Differential Input Amplifier Figure 27. Temperature Sensing Servo System heat/air conditioner modulator door in a duct system. Figure 28. Bridge Amplifier
3 VRef
Figure 29. Remote Latched Shutdown reset the over–current latch. Figure 30. Power H–Switch Buffer
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6.0 V for 100 kPa
2.0 V for Zero
Figure 31. Adjustable Pressure Differential Regulator
Figure 32. Switching Motor Controller With Buffered Output and Tach Feedback
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Figure 33. Switching Motor Controller With Buffered Output and Back EMF Sensing
15MOTOROLA ANALOG IC DEVICE DATA P SUFFIX PLASTIC PACKAGE CASE 648C–03 (DIP–16) DW SUFFIX PLASTIC PACKAGE CASE 751G–02 (SOP–16L) 916 MIN MIN MAX MAX MILLIMETERS INCHES DIM A B C D F G J K M P R 10.15 7.40 2.35 0.35 0.50 0.25 0.10 10.05 0.25 10.45 7.60 2.65 0.49 0.90 0.32 0.25 10.55 0.75 0.400 0.292 0.093 0.014 0.020 0.010 0.004 0.395 0.010 0.411 0.299 0.104 0.019 0.035 0.012 0.009 0.415 0.029 1.27 BSC 0.050 BSC –A– –B– P 8 PL G 14 PL –T– D 16 PL K C SEATING PLANE M R X 45° 0.25 (0.010) BM M 0.25 (0.010) T A BM S S NOTES: 1. DIMENSIONING AND TOLERANCING PER ANSI Y14.5M, 1982. 2. CONTROLLING DIMENSION: MILLIMETER. 3. DIMENSIONS A AND B DO NOT INCLUDE MOLD PROTRUSION. 4. MAXIMUM MOLD PROTRUSION 0.15 (0.006) PER SIDE. 5. DIMENSION D DOES NOT INCLUDE DAMBAR PROTRUSION. ALLOWABLE DAMBAR PROTRUSION SHALL BE 0.13 (0.005) TOTAL IN EXCESS OF D DIMENSION AT MAXIMUM MATERIAL CONDITION. F J 0.13 (0.005) T AM S 0.13 (0.005) T BM S MIN MIN MAX MAX MILLIMETERS DIM A B C D E F G J K L M N NOTES: 1. DIMENSIONING AND TOLERANCING PER ANSI Y14.5M, 1982. 2. CONTROLLING DIMENSION: INCH. 3. DIMENSION L TO CENTER OF LEADS WHEN FORMED PARALLEL. 4. DIMENSION B DOES NOT INCLUDE MOLD FLASH. 5. INTERNAL LEAD CONNECTION, BETWEEN 4 AND 5, 12 AND 13. 18.80 6.10 3.69 0.38 1.02 0.20 2.92 0.39 21.34 6.60 4.69 0.53 1.78 0.38 3.43 1.01 0.740 0.240 0.145 0.015 0.040 0.008 0.115 0.015 0.840 0.260 0.185 0.021 0.070 0.015 0.135 0.040
1.27 BSC
2.54 BSC
7.62 BSC
0.050 BSC
0.100 BSC
0.300 BSC
–A– –B– 916 NOTE 5 –T– SEATING PLANE F E G D 16 PL N K C L M J 16 PL INCHES OUTLINE DIMENSIONS
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