Method of converting an analog signal to digital signal by digitalizing error deviation

Information

  • Patent Grant
  • 6278388
  • Patent Number
    6,278,388
  • Date Filed
    Wednesday, September 15, 1999
    24 years ago
  • Date Issued
    Tuesday, August 21, 2001
    22 years ago
Abstract
It is an object of this invention to provide a digital conversion method for an analog signal in which, when sin(θ−φ) is calculated as a error deviation ε, a first output signal sin(θ−φ)·f(t) of the previous stage of the error deviation ε is converted into a digital signal by positive/negative sign determination performed by a comparator to make almost circuits into digital circuits, thereby making it easy to form an IC. In the digital conversion method for an analog signal according to the invention, sin(θ−φ)·f(t) obtained by guiding the rotation detection signal to a multiplier and operating the rotation detection signal is converted into a digital signal by positive/negative sign determination performed by a comparator to achieve a stable and inexpensive configuration.
Description




BACKGROUND OF THE INVENTION




1. Field of the Invention




The present invention relates to a digital conversion method for an analog signal and, more particularly, to an improvement in conversion performances (stability, high-speed performance, and noise resistance) by converting a first output signal sin(θ−φ)·f(t) into a digital signal by positive/negative sign determination performed by a comparator when sin(θ−φ) is calculated as an error deviation ε and a novel improvement for advantaging formation of a monolithic IC by reducing analog circuits in number.




2. Description of the Related Art




As a conventionally used digital conversion method for an analog signal of this type, for example, a tracking method shown in

FIG. 1

is popularly used. More specifically, as shown in

FIG. 1

, reference numeral


1


denotes a resolver excited by an exciting signal (i.e., reference signal) E·sin ωt. Two-phase outputs KEsin θsin ωt and KEcos θsin ωt output from the resolver


1


are operated by an operation unit


2


, and a two-phase output signal KEsinwtsin(θ−φ) (where θ is a resolver rotation angle, and φ is an output counter value) output from the operation unit


2


is synchronously rectified by a synchronous rectifier


3


to which the exciting signal E·sin ωt is input.




An output signal KEsin(θ−φ) obtained from the synchronous rectifier


3


is input to a counter


5


as a pulse output


4




a


through a voltage controlled oscillator


4


, in order to obtain an output counter value φ serving as a digital angle output from the counter


5


.




The output counter value φ is fed back, and thus a feed back loop is formed. Therefore, a velocity signal


6


is obtained by the output signal KEsin(θ−φ) from the synchronous rectifier


3


, and a position signal


7


can be obtained from the output counter value φ of the counter


5


.




The conventional digital conversion method for an analog signal has the configuration described above, the following problem is posed.




More specifically, since each constituent portion in the circuit configuration described above is partially constituted by a complex analog configuration, the entire configuration cannot be easily formed by an integrated monolithic semiconductor, and an exciting circuit or the like is inevitably added as a discrete part. For this reason, a low price, a reduction in size and weight, high reliability, and utility cannot be easily achieved. In addition, a preferable improvement means for a tracking speed is not found.




SUMMARY OF THE INVENTION




The present invention has been made to solve the above problem, and has as its object to, more particularly, a digital conversion method for an analog signal in which an improvement in conversion performances (stability, high-speed performance, and noise resistance) by converting a first output signal sin(θ−φ)·f(t) into a digital signal by positive/negative sign determination performed by a comparator when sin(θ−φ) is calculated as an error deviation e and an improvement for advantaging formation of a monolithic IC by reducing analog circuits in number.




A digital conversion method for an analog signal according to the present invention is a method for obtaining a digital angle output (φ) from rotation detection signals [sin θ·f(t) and cos θ·f(t): where f(t) is an exciting component] obtained from a rotation detector, wherein the rotation detection signals [sin θ·f(t) and cos θ·(t)] are guided to a multiplier and mutually operated with sin φ and cos φ obtained from the digital angle output (φ), in order to obtain [sin θ·f(t)×cos φ]−[cos θ·f(t)·sin φ]=sin(θ−φ)·f(t) as a first output signal, and the first output signal sin(θ−φ)·f(t) is converted into a digital signal by positive/negative sign determination performed by a comparator when the first output signal sin(θ−φ)·f(t) is synchronously detected to remove the exciting component f(t) and to obtain a second output signal sin(θ−φ) as an error deviation ε. The method is a method wherein the error deviation ε is input to a counter as a digital angular velocity signal ω(−φdot) through a compensator to be counted, and a digital angle output (φ) is obtained from the counter. The method is a method wherein, in a multiplier, sin and cos 10-bit multiplying DIA converters are used, and a 12-bit counter is used as the counter. The method is a method wherein the digital angle output (φ) is fed back and input to the sin and cos 10-bit multiplying D/A converters through a sin ROM and a cos ROM, and nonlinear characteristics are written in the sin ROM and the cos ROM. The method is a method wherein a DC bias current is applied to an output winding for outputting the rotation detection signals [sin θ·f(t) and cos θ·f(t)] depending on rotation of a rotor of the rotation detector, and a disconnection detection signal having a voltage higher than the maximum voltage of the rotation detection signals [sin θ·f(t) and cos θ·f(t)] from a differential amplifier when the output winding is disconnected. In addition, the method is a method wherein a phase difference between an exciting component included in the rotation detection signals sin θ·f(t) and cos θ·f(t) and an exciting signal of the rotation detector is detected, leading and trailing edges of the rotation detection signal component are detected to cause a reference signal guided to a synchronous detector to be synchronized with the exciting component included in the rotation detection signals.











BRIEF DESCRIPTION OF THE DRAWINGS





FIG. 1

is a block diagram of a conventional configuration.





FIG. 2

is a block diagram of a digital conversion method for an analog signal according to the present invention.





FIG. 3

is a schematic functional diagram showing functions in FIG.


2


.





FIG. 4

is a 4-phase divided operation waveform chart of an error deviation operation in FIG.


2


.





FIG. 5

is a block diagram of the error deviation operation in FIG.


2


.





FIG. 6

is an equivalent circuit of a compensator in FIG.


2


.





FIG. 7

is an equivalent circuit showing an operation of Z


−1


in FIG.


6


.





FIG. 8

is an equivalent circuit of a counter in FIG.


2


.





FIG. 9

is a block diagram showing another embodiment of the present invention.





FIG. 10

is a waveform chart of the operation in FIG.


9


.





FIG. 11

is a diagram showing a main part of

FIG. 2

according to the present invention.











DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS




Preferred embodiments of a digital conversion method for an analog signal according to the present invention will be described below with reference to the accompanying drawings.





FIG. 2

is a block diagram showing a digital tracking R/D converter to which the digital conversion method for an analog signal according to the present invention is applied.




In

FIG. 2

, reference numeral


1


denotes a rotation detector constituted by a resolver or a synchro. An exciting signal (component) f(t) serving as a reference signal sin ωt consisting of a 10-kHz sin wave from an exciting signal generator


50


of a digital tracking R/D (resolver/digital) converter


100


is applied to an exciting winding (not shown) of the rotation detector


1


. Two-phase rotation detection signals sin θ·f(t) and cos θ·f(t) are input from a two-phase output winding (not shown) to a sin 10-bit multiplying D/A converter 51 and a cos 10-bit multiplying D/A converter 52 depending on rotation of a rotor (not shown).




Outputs sin θ·f(t)·cos φ and cos θ·f(t)·sin φ (as will be described later, sin φ and cos φ of a digital angle output φ are fed back and input to the converters


51


and


52


through a sin ROM


60


and a cos ROM


61


, respectively) from the 10-bit multiplying D/A converters


51


and


52


are subtracted from each other {[sin θ·f(t)·cos φ]−[cos θ·f(t)·sin φ]=sin(θ−φ)·f(t)} by a subtractor


53


to obtain a first output signal sin(θ−φ)·f(t). This first output signal sin(θ−φ)·f(t) is subjected to positive/negative sign determination by a comparator


54


to be input to a synchronous detector


55


. The first output signal is synchronously detected by a reference signal f(t) from a synchronous phase detection disconnection detector


62


, an error deviation ε=sin(θ−φ) serving as a second output signal is counted by a 12-bit counter


57


through a compensator


56


, and the digital angle output φ is output as a parallel output


58




a


through a parallel interface


58


.




The digital angle output φ is output as a serial output


59




a


through a serial interface


59


, and pulse outputs


63




a


having known A, B, and Z phases and U, V, and W phases required to control a motor or the like are output by a pulse output generation logic


63


. At the same time, as described above, digital angle outputs φ are input to the sin ROM


60


and the cos ROM


61


in which required nonlinear characteristics are written in advance to output sin φ and cos φ,respectively. A multiplier (error deviation operation unit)


200


is constituted by the converters


51


and


52


, the subtractor


53


, and the comparator


54


.




In addition, a disconnection detection signal


62




a


output from the synchronous phase detection disconnection detector


62


is determined by a self-diagnosis unit


70


, and then input to a system controller


80


. The system controller


80


is designed to perform signal setting or outputting such as resolution setting, setting of U, V, and W poles, self-diagnosis outputting, outputting of an input/output control signal, and outputting of a system control signal.




Before concrete explanation of the respective parts in

FIG. 2

, the basic function of the present invention will be described below. The basic function is shown in FIG.


3


. More specifically, rotation detection signals sin θ·f(t) and cos θ·f(t) from the rotation detector


1


constituted by a resolver or a synchro are input to the error deviation operation unit


200


serving as a multiplier. The basic function is constituted by the compensator


56


for processing an obtained error deviation ε=sin(θ−φ) and the counter


57


serving as an object to be controlled.




Therefore, the rotation detection signals are given respectively:






sin θ·


f


(


t


), cos θ·


f


(


t


)  (1)






where θ is a rotation angle of the resolver


1


, and f(t) is an exciting component.




In this case, the error deviation ε is calculated by the error deviation operation unit


200


, tracking is performed to make the error deviation ε zero, thereby performing R/D conversion. More specifically,






[sin θ·


f


(


t


)×cos φ]−[cos θ·


f


(


t


)×sin φ]








=(sin θ·cos φ−cos θ·sinφ)·


f


(


t


)








=sin(θ−φ)·


f


(


t


)  (2)






In this equation (2), the term f(t) can be omitted by synchronous detection.






Therefore, ε=sin(θ−φ)  (3)






Thus, to establish ε=0 in the control system, θ=φ is obtained, and then the digital conversion is established. The basic function in the conventional method is the same as that in the method of the present invention. However, in the present invention, the value (analog quantity and size) of the error deviation itself is not considered. The function of the present invention is considerably different from the function of the conventional method in that the result of the equation (2) is only quantized (digitalized) by positive/negative sign determination using the comparator


54


(actually constituted by one pair of comparators as shown in FIG.


5


).




In the embodiment shown in

FIG. 2

, the RID converter having a resolution of 12 bits, and 12-bit converters are not used, but 10-bit converters are used as the multiplying DIA converters


51


and


52


serving as sin and cos multipliers which perform an operation in the error deviation operation unit


200


.




This is because, as will be described later, one rotation of 360° is divided into four phases each having 90°, and an operation process is repeated every 90° to simplify the hardware configuration of the circuit.




More specifically, the angle of 90° corresponds to 10 bits in a 12-bit RID converter. In addition, since digital processing is performed, degradation of performance can also be avoided even if the f our-phase dividing method for simplifying the circuit.




A method of calculating the error deviation ε by four-phase division will be described below. Operation waveforms obtained by the four-phase division are operations of quadrants PH1 to PH4 in FIG.


4


. When the operations are expressed by a table, the first table of Table 1 is obtained.












TABLE 1











First Table














Quadrant




Range




Error Deviation




Remark









I




 0°˜90°




ε = sinθ · cosφ − cosθ · sinφ




PH1






II




 90°˜180°




ε = −(sinθ · {overscore (cosφ)} + cosθ · sinφ




PH2






III




180°˜270°




ε = −(sinθ · {overscore (cosφ)} − cosθ · {overscore (sinφ)}




PH3






IV




270°˜360°




ε = sinθ · cosφ + cosθ · {overscore (sinφ)}




PH4














The error deviation operation circuit


200


is as shown in FIG.


5


. The subtractor


53


and the comparator


54


shown in

FIG. 2

are constituted by one pair of subtractors and one pair of comparators, respectively. In each of the comparators


54


, positive/negative sign determination of an output from each of the subtractors


53


, four-phase operations are sequentially performed by gates G


1


to G


4


in each of the quadrants PH1 to PH4, and an error deviation δ is obtained from a gate G


6


to which the reference signal f(t) is input.




The compensator


56


is constituted like an equivalent circuit shown in FIG.


6


. An object to be controlled by the digital tracking R/D converter according to the present invention is the counter


57


, and the digital tracking R/D converter has primary integral characteristics. For this reason, in order to realize feedback control systems of two types as means for stably controlling the counter


57


, serving as the object to be controlled, at a high speed and a high accuracy, the characteristics of the compensator


56


are given by PI (proportion+integration), and the compensator


56


is combined to a first-order-lag filter (Tf is a first-order-lag filter time constant). The compensator


56


in

FIG. 6

is expressed by the following equation (4):








K


(


s


)=(


Kp+Ki/S


)×1/(1


+Tf·S


)  (4)






where:




S is Laplacean;




1/(1+Tf·S) is a first-order-lag filter; and




ΔT is an operation-clock cycle.




Although KFB and KFF are not included in the equation (4), KFB is set to assure/improve stability in a static state, and KFF is set to assure/improve high-speed response. KFB and KFF are properly used in embodiments.




Z


−1


represents a previous value which is latch data one clock cycle before a present value when data update is performed every clock cycle (ΔT) as shown in FIG.


7


. This state is as shown in FIG.


7


.




The counter


57


serving as the object to be controlled has the 12-bit configuration as described above, and is constituted by a known adder and a known subtractor for integrating an angular velocity ω(=φdot) obtained by the compensator


56


of the previous stage. The counter


57


is represented by an equivalent circuit shown in

FIG. 8

, and performs a count operation by an operation clock cycle ΔT.




As the method according to the present invention, a method of automatically correcting the phases between the rotation detection signals sin θ·f(t) and cos θ·f(t) shown in FIG.


9


and

FIG. 10

can be applied.

FIG. 9

is a block diagram, and

FIG. 10

is a waveform chart.




In

FIG. 9

, rotation detection signals sin θ·f(t) and cos θ·f(t) consist of analog rotation detection signals having exciting components f(t) from the rotation detector


1


. The rotation detection signals sin θ·f(t) and cos θ·f(t) are input to an absolute value comparator


10


and connected to first and second terminals


12


and


13


of a switch means


11


.




An edge detector


14


for detecting leading and trailing edges are connected to a switching contact


11




a


of the switch means


11


, and an edge output


14




a


from the edge detector


14


is input to a synchronizing circuit


15


.




In this case, the exciting component f(t) of the rotation detection signal is given by f(t)=sin(ωt+Δω) in consideration of a phase difference Δω between the exciting component f(t) and a reference exciting signal, and the reference exciting signal is given by f(t)=sinωt.




The reference exciting signal f(t) supplied to the rotation detector


1


is input to a 90°·270° signal generator


16


and a phase adjustment region setting unit


17


.




An output


17




a


from the phase adjustment region setting unit


17


is input to the synchronizing circuit


15


, and a new reference signal


3




a


obtained by correcting sin(ωt+Δω) obtained by phase-shifting sin ωt of the reference exciting signal f(t) by Δω is obtained by the synchronizing circuit


15


.




A case wherein automatic phase correction is actually performed will be described below.




As shown in

FIG. 10

, the waveform of the reference exciting signal f(t) is shaped to check a reference phase, and a 90° trigger


16




a


and a 270° trigger


16




b


are output from the 90°-270° signal generator


16


. A polarity signal


20


is formed by the phase adjustment region setting unit


17


, and a trigger output


14




a


and a phase difference Δω of the rotation detection signals sin θ·f(t) and cos θ·f(t) are detected. When the waveforms of the rotation detection signals sin θ·f(t) and cos θ·f(t) are shaped, a rotation detection signal phase (reference component phase)


3




b


A is obtained.




The new reference signal


3




a


synchronized by the trigger output


14




a


is obtained. When the new reference signal


3




a


is used as an exciting signal, the rotation detection signals sin θ·f(t) and cos θ·f(t) and the new reference signal


3




a


can be synchronized with each other, and the phase difference Δω generated by the rotation detector itself, a cable impedance, a change in temperature, and the like can be automatically corrected.




When the phase difference Δω described above is automatically corrected, as a phase-adjustable range, a range of a phase difference of about ±90° can be used.




The method shown in

FIG. 11

represents a concrete example of a disconnection detection method of the rotation detector


1


shown in FIG.


2


. More specifically, the rotation detector


1


in

FIG. 11

constituted by a resolver constituted by an exciting winding


1


A and an output winding


1


B. Since the output winding


1


B has two-phase outputs, the output winding


1


B is constituted by one pair of windings. However, one winding will be omitted, and only the output winding


1


B for outputting sin or cos signal will be described below.




An operation amplifier


8


is connected to input lines


300


and


301


, connected to both the terminals of the output winding


1


B, through first and second resistors R


1


and R


3


, a common terminal COM is connected to a positive-phase terminal


8




a


of the operation amplifier


8


through a third resistor R


2


, and a fourth resistor R


4


is connected between a negative-phase terminal


8




b


and an output terminal


8




c.


A known differential amplifier


350


is constituted by the operation amplifier


8


and the resistors R


1


to R


4


described above, so that the rotation detection signal sin θ·f(t) or cos θ·f(t) is output from the output terminal


8




c.






Fifth and sixth resistors R


SU


and R


SL


having equal resistances are connected to the input lines


300


and


301


, respectively, and a DC bias current I


B


from a DC power source


351


is applied to flow from the fifth resistor R


BU


to the sixth resistor R


BL


through the output winding


1


B. Note that the DC bias current I


B


is set not to adversely affect the voltage level of the rotation detection signal sin θ·f(t) or cos θ·f(t).




An operation will be described below. When the output winding


1


B is normal without being disconnected, the rotation detection signal sin θ·f(t) or cos θ·f(t) excited by the output winding


1


B is output from the output terminal


8




c


through the differential amplifier


350


. When the output winding


1


B is disconnected, the DC bias current I


B


does not flow in the output winding


1


B and the sixth resistor R


BL


, and, at the same time, the voltage of the DC power source


351


is applied to the differential amplifier


350


to output a disconnection detection signal


400


in place of the rotation detection signal sin θ·f(t) or cos θ·f(t). The disconnection detection signal


400


has a voltage (for example, 5 V) higher than the voltage of the rotation detection signal sin θ·f(t) or cos θ·f(t). When the voltage level of the disconnection detection signal


400


is monitored by, a known window comparator or the like, the presence/absence of disconnection can be detected.




Since the digital conversion method for an analog signal according to the present invention has the configuration described above, the following advantages can be obtained.




More specifically, when sin(θ−φ) is calculated as a error deviation ε, a first output signal sin(θ−φ)·f(t) of the previous stage of the error deviation ε is converted into a digital signal by positive/negative sign determination performed by a comparator. The digital signal is input to a counter to obtain a digital angle output. For this reason, an R/D conversion process can be digitized, and improvements in conversion performances (stability, high-speed performance, and noise resistance) can be obtained.




When analog circuits are reduced in number, formation of a monolithic IC is advantaged, and products each having high reliability, a small size, and a low price can be manufactured (mass-production).




Since disconnection of a winding of a rotation detector can also be detected, an improvement in reliability can be achieved.




In addition, since a phase between a rotation detection signal and an exciting signal (reference signal) can be automatically corrected, detection accuracy can be improved and stabilized.



Claims
  • 1. A digital conversion method for an analog signal for obtaining a digital angle output (φ) from rotation detection signals [sin θ·f(t) and cos θ·f(t): where f(t) is an exciting component] detected by a rotation detector, wherein the rotation detection signals [sin θ·f(t) and cos θ·f(t)] are guided to a multiplier and mutually operated with sin φ and cos φ derived from the digital angle output (φ) to obtain [sin θ·f(t)×cos φ]−[cos θ·f(t)×sin φ]=sin(θ−φ)·f(t) as a first output signal, and the first output signal sin(θ−φ)·f(t) is converted into a digital signal by positive/negative sign determination performed by a comparator when the first output signal sin(θ−φ)·f(t) is synchronously detected to remove the exciting component f(t) and to obtain a second output signal sin(θ−φ) as an error deviation ε.
  • 2. A digital conversion method for an analog signal according to claim 1, wherein the error deviation ε is input to a counter as a digital angular velocity signal ω(=φdot) through a compensator to be counted, and a digital angle output (φ) is obtained from the counter.
  • 3. A digital conversion method for an analog signal according to claim 2, wherein, in a multiplier, sin and cos 10-bit multiplying D/A converters are used, and a 12-bit counter is used as the counter.
  • 4. A digital conversion method for an analog signal according to claim 3, wherein the digital angle output (φ) is fed back and input to the sin and cos 10-bit multiplying D/A converters through a sin ROM and a cos ROM, and nonlinear characteristics are written in the sin ROM and the cos ROM.
  • 5. A digital conversion method for an analog signal according to claim 4, wherein a DC bias current is applied to an output winding for outputting the rotation detection signals [sin θ·f(t) and cos θ·f(t)] depending on rotation of a rotor of the rotation detector, and a disconnection detection signal having a voltage higher than the maximum voltage of the rotation detection signals [sin θ·f(t) and cos θ·f(t)] are output from a differential amplifier when the output winding is disconnected.
  • 6. A digital conversion method for an analog signal according to claim 4, wherein a phase difference between an exciting component included in the rotation detection signals sin θ·f(t) and cos θ·f(t) and an exciting signal of the rotation detector is detected, leading and trailing edges of the exciting components f(t) of the rotation detection signals sin θ·f(t) and cos θ·f(t) are detected to cause a reference signal f(t) guided to a synchronous detector to be synchronized with the exciting component f(t) included in the rotation detection signals sin θ·f(t) and cos θ·f(t).
  • 7. A digital conversion method for an analog signal according to claim 3, wherein a DC bias current is applied to an output winding for outputting the rotation detection signals [sin θ·f(t) and cos θ·f(t)] depending on rotation of a rotor of the rotation detector, and a disconnection detection signal having a voltage higher than the maximum voltage of the rotation detection signals [sin θ·f(t) and cos θ·f(t)] are output from a differential amplifier when the output winding is disconnected.
  • 8. A digital conversion method for an analog signal according to claim 3, wherein a phase difference between an exciting component included in the rotation detection signals sin θ·f(t) and cos θ·f(t) and an exciting signal of the rotation detector is detected, leading and trailing edges of the exciting components f(t) of the rotation detection signals sin θ·f(t) and cos θ·f(t) are detected to cause a reference signal f(t) guided to a synchronous detector to be synchronized with the exciting component f(t) included in the rotation detection signals sin θ·f(t) and cos θ·f(t).
  • 9. A digital conversion method for an analog signal according to claim 2, wherein the digital angle output (φ) is fed back and input to the sin and cos 10-bit multiplying DIA converters through a sin ROM and a cos ROM, and nonlinear characteristics are written in the sin ROM and the cos ROM.
  • 10. A digital conversion method for an analog signal according to claim 9, wherein a DC bias current is applied to an output winding for outputting the rotation detection signals [sin θ·f(t) and cos θ·f(t)] depending on rotation of a rotor of the rotation detector, and a disconnection detection signal having a voltage higher than the maximum voltage of the rotation detection signals [sin θ·f(t) and cos θ·f(t)] are output from a differential amplifier when the output winding is disconnected.
  • 11. A digital conversion method for an analog signal according to claim 9, wherein a phase difference between an exciting component included in the rotation detection signals sin θ·f(t) and cos θ·f(t) and an exciting signal of the rotation detector is detected, leading and trailing edges of the exciting components f(t) of the rotation detection signals sin θ·f(t) and cos θ·f(t) are detected to cause a reference signal f(t) guided to a synchronous detector to be synchronized with the exciting component f(t) included in the rotation detection signals sin θ·f(t) and cos θ·f(t).
  • 12. A digital conversion method for an analog signal according to claim 2, wherein a DC bias current is applied to an output winding for outputting the rotation detection signals [sin θ·f(t) and cos θ·f(t)] depending on rotation of a rotor of the rotation detector, and a disconnection detection signal having a voltage higher than the maximum voltage of the rotation detection signals [sin θ·f(t) and cos θ·f(t)] are output from a differential amplifier when the output winding is disconnected.
  • 13. A digital conversion method for an analog signal according to claim 2, wherein a phase difference between an exciting component included in the rotation detection signals sin θ·f(t) and cos θ·f(t) and an exciting signal of the rotation detector is detected, leading and trailing edges of the exciting components f(t) of the rotation detection signals sin θ·f(t) and cos θ·f(t) are detected to cause a reference signal f(t) guided to a synchronous detector to be synchronized with the exciting component f(t) included in the rotation detection signals sin θ·f(t) and cos θ·f(t).
  • 14. A digital conversion method for an analog signal according to claim 1, wherein, in a multiplier, sin and cos 10-bit multiplying D/A converters are used, and a 12-bit counter is used as the counter.
  • 15. A digital conversion method for an analog signal according to claim 14, wherein the digital angle output (φ) is fed back and input to the sin and cos 10-bit multiplying D/A converters through a sin ROM and a cos ROM, and nonlinear characteristics are written in the sin ROM and the cos ROM.
  • 16. A digital conversion method for an analog signal according to claim/, wherein a DC bias current is applied to an output winding for outputting the rotation detection signals [sin θ·f(t) and cos θ·f(t)] depending on rotation of a rotor of the rotation detector, and a disconnection detection signal having a voltage higher than the maximum voltage of the rotation detection signals [sin θ·f(t) and cos θ·f(t)] are output from a differential amplifier when the output winding is disconnected.
  • 17. A digital conversion method for an analog signal according to claim 15, wherein a phase difference between an exciting component included in the rotation detection signals sin θ·f(t) and cos θ·f(t) and an exciting signal of the rotation detector is detected, leading and trailing edges of the exciting components f(t) of the rotation detection signals sin θ·f(t) and cos θ·f(t) are detected to cause a reference signal f(t) guided to a synchronous detector to be synchronized with the exciting component f(t) included in the rotation detection signals sin θ·f(t) and cos θ·f(t).
  • 18. A digital conversion method for an analog signal according to claim 14, wherein a DC bias current is applied to an output winding for outputting the rotation detection signals [sin θ·f(t) and cos θ·f(t)] depending on rotation of a rotor of the rotation detector, and a disconnection detection signal having a voltage higher than the maximum voltage of the rotation detection signals [sin θ·f(t) and cos θ·f(t)] are output from a differential amplifier when the output winding is disconnected.
  • 19. A digital conversion method for an analog signal according to claim 14, wherein a phase difference between an exciting component included in the rotation detection signals sin θ·f(t) and cos θ·f(t) and an exciting signal of the rotation detector is detected, leading and trailing edges of the exciting components f(t) of the rotation detection signals sin θ·f(t) and cos θ·f(t) are detected to cause a reference signal f(t) guided to a synchronous detector to be synchroniized with the exciting component f(t) included in the rotation detection signals sin θ·f(t) and cos θ·f(t).
  • 20. A digital conversion method for an analog signal according to claim 1, wherein the digital angle output (φ)is fed back and input to the sin and cos 10-bit multiplying DIA converters through a sin ROM and a cos ROM, and nonlinear characteristics are written in the sin ROM and the cos ROM.
  • 21. A digital conversion method for an analog signal according to claim 20, wherein a DC bias current is applied to an output winding for outputting the rotation detection signals [sin θ·f(t) and cos θ·f(t)] depending on rotation of a rotor of the rotation detector, and a disconnection detection signal having a voltage higher than the maximum voltage of the rotation detection signals [sin θ·f(t) and cos θ·f(t)] are output from a differential amplifier when the output winding is disconnected.
  • 22. A digital conversion method for an analog signal according to claim 20, wherein a phase difference between an exciting component included in the rotation detection signals sin θ·f(t) and cos θ·f(t) and an exciting signal of the rotation detector is detected, leading and trailing edges of the exciting components f(t) of the rotation detection signals sin θ·f(t) and cos θ·f(t) are detected to cause a reference signal f(t) guided to a synchronous detector to be synchronized with the exciting component f(t) included in the rotation detection signals sin θ·f(t) and cos θ·f(t).
  • 23. A digital conversion method for an analog signal according to claim 1, wherein a DC bias current is applied to an output winding for outputting the rotation detection signals [sin θ·f(t) and cos θ·f(t)] depending on rotation of a rotor of the rotation detector, and a disconnection detection signal having a voltage higher than the maximum voltage of the rotation detection signals [sin θ·f(t) and cos θ·f(t)] are output from a differential amplifier when the output winding is disconnected.
  • 24. A digital conversion method for an analog signal according to claim 1, wherein a phase difference between an exciting component included in the rotation detection signals sin θ·f(t) and cos θ·f(t) and an exciting signal of the rotation detector is detected, leading and-trailing edges of the exciting components f(t) of the rotation detection signals sin θ·f(t) and cos θ·f(t) are detected to cause a reference signal f(t) guided to a synchronous detector to be synchronized with the exciting component f(t) included in the rotation detection signals sin θ·f(t) and cos θ·f(t).
Priority Claims (1)
Number Date Country Kind
11-165370 Jun 1999 JP
US Referenced Citations (4)
Number Name Date Kind
5079549 Liessner Jan 1992
5189353 Ezuka Feb 1993
5796357 Kushihara Aug 1998
5949359 Vlahu Sep 1999