Method and device for monitoring an actuator system
First Claim
1. A method for monitoring an actuator in a physical system, the method comprising:
- monitoring, based on measured system quantities, the actuator, via a processor having a computer model that describes the actuator, the behavior of the actuator being represented by a computer model function and one or more parameters of the computer model function;
determining or adapting values of the parameters of the computer model with the aid of one or more particular system quantities;
determining an error when a specified error condition is fulfilled, the error condition defining when at least one of the parameters, and/or at least one quantity determined from a plurality of the parameters, lies outside a corresponding specified target deviation range for a relevant parameter or the relevant quantity; and
determining that a component of the actuator is faulty if the error is determined;
wherein the actuator includes an electromechanical throttle valve actuator for a throttle valve in an engine system having an internal combustion engine, the position of the throttle valve and/or an electric voltage applied to the electromechanical throttle valve actuator being specified as the system quantities, andwherein for the actuator, the error condition on the basis of which a particular error can be identified include at least one of the following error types;
(i) an actuator spring is broken and/or missing, and/or a low resistance, and/or a short-circuit, and/or a weak motor, and/or defective permanent magnets;
(ii) an actuator friction is too high due to contamination and/or stiffness;
(iii) an actuator friction is too low due to wear, missing shaft sealant, and/or a broken coupling bar;
(iv) an actuator component has a high resistance; and
(v) the actuator component has a low resistance due to a short circuit, a weak motor, and/or defective permanent magnets, andwherein error types (i) correspond to the following error condition;
α
>
S(α
)+Δ
α
&
η
/α
<
S(η
/α
)−
Δ
(η
/α
),wherein error types (ii) correspond to the following error conditions;
S(α
)−
Δ
α
<
α
<
S(α
)+Δ
α
&
μ
/α
>
S(μ
/α
)+Δ
(μ
/α
)&
S(η
/α
)−
Δ
(η
/α
)<
η
/α
<
S(η
/α
)+Δ
(η
/α
),wherein error types (iii) correspond to the following error conditions;
S(α
)−
Δ
α
<
α
<
S(α
)+Δ
α
&
μ
/α
<
S(μ
/α
)−
Δ
(μ
/α
)&
S(η
/α
)−
Δ
(η
/α
)<
η
/α
<
S(η
/α
)+Δ
(η
/α
),wherein error types (iv) correspond to the following error conditions;
η
/α
>
S(η
/α
)+Δ
(η
/α
)
(α
<
S(α
)−
Δ
α
&
μ
/α
>
S(μ
/α
)+Δ
(μ
/α
), andwherein error types (v) correspond to the following error conditions;
α
>
S(α
)+Δ
α
&
μ
/α
<
S(μ
/α
)−
Δ
(μ
/α
),where R is a winding resistance of an actuator drive of the actuator, L is an inductance of a winding of the actuator drive, I represents an actuator current through the actuator drive, J represents a mass moment of inertia, and Cm and Kgear represent a gear ratio,
1 Assignment
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Accused Products
Abstract
A method for monitoring an actuator in a physical system, including: providing a computer model that describes the actuator, the behavior of the actuator being represented by a computer model function and by one or more parameters of the computer model function; determining or adapting the values of the parameters of the computer model with the aid of one or more particular system quantities; determining an error when a specified error condition is fulfilled, the error condition defining when at least one of the parameters, and/or at least one quantity determined from a plurality of the parameters, lies outside a corresponding specified target deviation range for the relevant parameter or the relevant quantity.
-
Citations
16 Claims
-
1. A method for monitoring an actuator in a physical system, the method comprising:
-
monitoring, based on measured system quantities, the actuator, via a processor having a computer model that describes the actuator, the behavior of the actuator being represented by a computer model function and one or more parameters of the computer model function; determining or adapting values of the parameters of the computer model with the aid of one or more particular system quantities; determining an error when a specified error condition is fulfilled, the error condition defining when at least one of the parameters, and/or at least one quantity determined from a plurality of the parameters, lies outside a corresponding specified target deviation range for a relevant parameter or the relevant quantity; and determining that a component of the actuator is faulty if the error is determined; wherein the actuator includes an electromechanical throttle valve actuator for a throttle valve in an engine system having an internal combustion engine, the position of the throttle valve and/or an electric voltage applied to the electromechanical throttle valve actuator being specified as the system quantities, and wherein for the actuator, the error condition on the basis of which a particular error can be identified include at least one of the following error types;
(i) an actuator spring is broken and/or missing, and/or a low resistance, and/or a short-circuit, and/or a weak motor, and/or defective permanent magnets;
(ii) an actuator friction is too high due to contamination and/or stiffness;
(iii) an actuator friction is too low due to wear, missing shaft sealant, and/or a broken coupling bar;
(iv) an actuator component has a high resistance; and
(v) the actuator component has a low resistance due to a short circuit, a weak motor, and/or defective permanent magnets, andwherein error types (i) correspond to the following error condition;
α
>
S(α
)+Δ
α
&
η
/α
<
S(η
/α
)−
Δ
(η
/α
),wherein error types (ii) correspond to the following error conditions;
S(α
)−
Δ
α
<
α
<
S(α
)+Δ
α
&
μ
/α
>
S(μ
/α
)+Δ
(μ
/α
)&
S(η
/α
)−
Δ
(η
/α
)<
η
/α
<
S(η
/α
)+Δ
(η
/α
),wherein error types (iii) correspond to the following error conditions;
S(α
)−
Δ
α
<
α
<
S(α
)+Δ
α
&
μ
/α
<
S(μ
/α
)−
Δ
(μ
/α
)&
S(η
/α
)−
Δ
(η
/α
)<
η
/α
<
S(η
/α
)+Δ
(η
/α
),wherein error types (iv) correspond to the following error conditions;
η
/α
>
S(η
/α
)+Δ
(η
/α
)
(α
<
S(α
)−
Δ
α
&
μ
/α
>
S(μ
/α
)+Δ
(μ
/α
), andwherein error types (v) correspond to the following error conditions;
α
>
S(α
)+Δ
α
&
μ
/α
<
S(μ
/α
)−
Δ
(μ
/α
),where R is a winding resistance of an actuator drive of the actuator, L is an inductance of a winding of the actuator drive, I represents an actuator current through the actuator drive, J represents a mass moment of inertia, and Cm and Kgear represent a gear ratio, - View Dependent Claims (2, 3, 4, 5, 6)
-
-
7. A device for monitoring an actuator in a physical system, which includes a control device for operating the physical system having the actuator, comprising:
-
a monitoring arrangement to monitor, based on measured system quantities, the actuator, via a processor having a computer model that describes the actuator, the behavior of the actuator being represented by a computer model function and one or more parameters of the computer model function; wherein the monitoring arrangement is configured to determine or adapt values of the parameters of the computer model with the aid of one or more particular system quantities, wherein the monitoring arrangement is configured to determine an error when a specified error condition is fulfilled, the error condition defining when at least one of the parameters, and/or at least one quantity determined from a plurality of the parameters, lies outside a corresponding specified target deviation range for a relevant parameter or the relevant quantity, wherein the monitoring arrangement is configured to determine that a component of the actuator is faulty if the error is determined, wherein the actuator includes an electromechanical throttle valve actuator for a throttle valve in an engine system having an internal combustion engine, the position of the throttle valve and/or an electric voltage applied to the electromechanical throttle valve actuator being specified as the system quantities, and wherein for the actuator, the error condition on the basis of which a particular error can be identified include at least one of the following error types;
(i) an actuator spring is broken and/or missing, and/or a low resistance, and/or a short-circuit, and/or a weak motor, and/or defective permanent magnets;
(ii) an actuator friction is too high due to contamination and/or stiffness;
(iii) an actuator friction is too low due to wear, missing shaft sealant, and/or a broken coupling bar;
(iv) an actuator component has a high resistance; and
(v) the actuator component has a low resistance due to a short circuit, a weak motor, and/or defective permanent magnets, andwherein error types (i) correspond to the following error condition;
α
>
S(α
)+Δ
α
&
η
/α
<
S(η
/α
)−
Δ
(η
/α
),wherein error types (ii) correspond to the following error conditions;
S(α
)−
Δ
α
<
α
<
S(α
)+Δ
α
&
μ
/α
>
S(μ
/α
)+Δ
(μ
/α
)&
S(η
/α
)−
Δ
(η
/α
)<
η
/α
<
S(η
/α
)+Δ
(η
/α
),wherein error types (iii) correspond to the following error conditions;
S(α
)−
Δ
α
<
α
<
S(α
)+Δ
α
&
μ
/α
<
S(μ
/α
)−
Δ
(μ
/α
)&
S(η
/α
)−
Δ
(η
/α
)<
η
/α
<
S(η
/α
)+Δ
(η
/α
),wherein error types (iv) correspond to the following error conditions;
η
/α
>
S(η
/α
)+Δ
(η
/α
)
(α
<
S(α
)−
Δ
α
&
μ
/α
>
S(μ
/α
)+Δ
(μ
/α
), andwherein error types (v) correspond to the following error conditions;
α
>
S(α
)+Δ
α
&
μ
/α
<
S(μ
/α
)−
Δ
(μ
/α
),where R is a winding resistance of an actuator drive of the actuator, L is an inductance of a winding of the actuator drive, I represents an actuator current through the actuator drive, J represents a mass moment of inertia, and Cm and Kgear represent a gear ratio, - View Dependent Claims (8)
-
-
9. An actuator system, comprising:
-
an actuator; and a device for monitoring an actuator in a physical system, which includes a control device for operating the physical system having the actuator, including; a monitoring arrangement to monitor, based on measured system quantities, the actuator, via a processor having a computer model that describes the actuator, the behavior of the actuator being represented by a computer model function and one or more parameters of the computer model function; wherein the monitoring arrangement is configured to determine or adapt values of the parameters of the computer model with the aid of one or more particular system quantities, wherein the monitoring arrangement is configured to determine an error when a specified error condition is fulfilled, the error condition defining when at least one of the parameters, and/or at least one quantity determined from a plurality of the parameters, lies outside a corresponding specified target deviation range for a relevant parameter or the relevant quantity, wherein the monitoring arrangement is configured to determine that a component of the actuator is faulty if the error is determined, and wherein the actuator includes an electromechanical throttle valve actuator for a throttle valve in an engine system having an internal combustion engine, the position of the throttle valve and/or an electric voltage applied to the electromechanical throttle valve actuator being specified as the system quantities, and wherein for the actuator, the error condition on the basis of which a particular error can be identified include at least one of the following error types;
(i) an actuator spring is broken and/or missing, and/or a low resistance, and/or a short-circuit, and/or a weak motor, and/or defective permanent magnets;
(ii) an actuator friction is too high due to contamination and/or stiffness;
(iii) an actuator friction is too low due to wear, missing shaft sealant, and/or a broken coupling bar;
(iv) an actuator component has a high resistance; and
(v) the actuator component has a low resistance due to a short circuit, a weak motor, and/or defective permanent magnets, andwherein error types (i) correspond to the following error condition;
α
>
S(α
)+Δ
α
&
η
/α
<
S(η
/α
)−
Δ
(η
/α
),wherein error types (ii) correspond to the following error conditions;
S(α
)−
Δ
α
<
α
<
S(α
)+Δ
α
&
μ
/α
>
S(μ
/α
)+Δ
(μ
/α
)&
S(η
/α
)−
Δ
(η
/α
)<
η
/α
<
S(η
/α
)+Δ
(η
/α
),wherein error types (iii) correspond to the following error conditions;
S(α
)−
Δ
α
<
α
<
S(α
)+Δ
α
&
μ
/α
<
S(μ
/α
)−
Δ
(μ
/α
)&
S(η
/α
)−
Δ
(η
/α
)<
η
/α
<
S(η
/α
)+Δ
(η
/α
),wherein error types (iv) correspond to the following error conditions;
η
/α
>
S(η
/α
)+Δ
(η
/α
)
(α
<
S(α
)−
Δ
α
&
μ
/α
>
S(μ
/α
)+Δ
(μ
/α
), andwherein error types (v) correspond to the following error conditions;
α
>
S(α
)+Δ
α
&
μ
/α
<
S(μ
/α
)−
Δ
(μ
/α
),where R is a winding resistance of an actuator drive of the actuator, L is an inductance of a winding of the actuator drive, I represents an actuator current through the actuator drive, J represents a mass moment of inertia, and Cm and Kgear represent a gear ratio, - View Dependent Claims (10)
-
-
11. A non-transitory computer readable medium having a computer program, which is executable by a processor, comprising:
-
a program code arrangement having program code for monitoring an actuator in a physical system, by performing the following; monitoring, based on measured system quantities, the actuator, via a processor having a computer model that describes the actuator, the behavior of the actuator being represented by a computer model function and one or more parameters of the computer model function; determining or adapting values of the parameters of the computer model with the aid of one or more particular system quantities; determining an error when a specified error condition is fulfilled, the error condition defining when at least one of the parameters, and/or at least one quantity determined from a plurality of the parameters, lies outside a corresponding specified target deviation range for a relevant parameter or the relevant quantity; and determining that a component of the actuator is faulty if the error is determined; wherein the actuator includes an electromechanical throttle valve actuator for a throttle valve in an engine system having an internal combustion engine, the position of the throttle valve and/or an electric voltage applied to the electromechanical throttle valve actuator being specified as the system quantities, and wherein for the actuator, the error condition on the basis of which a particular error can be identified include at least one of the following error types;
(i) an actuator spring is broken and/or missing, and/or a low resistance, and/or a short-circuit, and/or a weak motor, and/or defective permanent magnets;
(ii) an actuator friction is too high due to contamination and/or stiffness;
(iii) an actuator friction is too low due to wear, missing shaft sealant, and/or a broken coupling bar;
(iv) an actuator component has a high resistance; and
(v) the actuator component has a low resistance due to a short circuit, a weak motor, and/or defective permanent magnets, andwherein error types (i) correspond to the following error condition;
α
>
S(α
)+Δ
α
&
η
/α
<
S(η
/α
)−
Δ
(η
/α
),wherein error types (ii) correspond to the following error conditions;
S(α
)−
Δ
α
<
α
<
S(α
)+Δ
α
&
μ
/α
>
S(μ
/α
)+Δ
(μ
/α
)&
S(η
/α
)−
Δ
(η
/α
)<
η
/α
<
S(η
/α
)+Δ
(η
/α
),wherein error types (iii) correspond to the following error conditions;
S(α
)−
Δ
α
<
α
<
S(α
)+Δ
α
&
μ
/α
<
S(μ
/α
)−
Δ
(μ
/α
)&
S(η
/α
)−
Δ
(η
/α
)<
η
/α
<
S(η
/α
)+Δ
(η
/α
),wherein error types (iv) correspond to the following error conditions;
η
/α
>
S(η
/α
)+Δ
(η
/α
)
(α
<
S(α
)−
Δ
α
&
μ
/α
>
S(μ
/α
)+Δ
(μ
/α
), andwherein error types (v) correspond to the following error conditions;
α
>
S(α
)+Δ
α
&
μ
/α
<
S(μ
/α
)−
Δ
(μ
/α
),where R is a winding resistance of an actuator drive of the actuator, L is an inductance of a winding of the actuator drive, I represents an actuator current through the actuator drive, J represents a mass moment of inertia, and Cm and Kgear represent a gear ratio, and where - View Dependent Claims (12, 13, 14, 15, 16)
-
Specification