DESIGN OF INTELLIGENT RESILIENT STRUCTURES VIA AUTOMATIC PLACEMENT OF SENSOR AND SMART ACTUATORS
An innovative method to automatically place sensors and stimuli-sensitive active actuators to neutralize the effects of structural faults and design a smart fault-resilient system is described. To the best of our knowledge, the proposed framework is the first systematic integration of thermally activated shape memory polymer actuators with a sensor distribution framework targeted to bring a damaged structural system to its native state. The framework does not explicitly model the material constitutive model and hence can be applied to linear and nonlinear material behaviors. The approach enables the design of resilient smart structures that can be additively manufactured. The framework computes a matrix of relative importance for different sensor positions and uses that to optimally place actuators to reconfigure the system in presence of faults.
1 . A computer-implemented method for placing sensors on an active resilient structure design, comprising:
receiving an initial design domain for a truss structure formed from a plurality of members connected by nodes, the members include passive structures and structures formed with stimuli sensitive actuators;
creating a mathematical array of sensor placement sensitivity by successively measuring, for each respective sensor disposed on a respective member of a plurality of members comprising the truss structure, a respective relative change in structural response based on applying respective faults on other members of the plurality of members other than the respective member;
iteratively using the mathematical array of sensor placement sensitivity to evaluate different locations for groups of sensors disposed on the plurality of members in the truss structure, to measure a change in the structural response until at least one of i) a predefined number of stimuli sensitive actuators is reached, ii) a predefined number of sensors is reached, iii) a predefined computational budget is reached, and iv) a predefined computational performance is reached;
identifying, based on the evaluation of different locations of each sensor, locations of a fewest number of sensors in the groups of sensors that produce a relatively larger measured change in the structural response for a given location of a fault; and
producing a design workflow to generate one or more active resilient structure designs based on the locations of the fewest number of sensors that produce the relatively larger measured change in the structural response, in order to neutralize the effects of a simulated fault on the truss structure.
2 . The computer-implemented method of claim 1 , wherein the receiving the initial design domain for a truss structure includes receiving the initial design with at least one of 1) boundary conditions and ii) loading conditions.
3 . The computer-implemented method of claim 1 , wherein the producing the design workflow to generate one or more designs of with placement of stimuli sensitive actuators includes at least one of i) actuators that change their shape in response to stimuli, ii) passive material that does not change its shape in response to stimuli, and iii) materials that have one or more voids.
4 . The computer-implemented method of claim 1 , wherein the producing the design workflow to generate one or more designs of with placement of stimuli sensitive actuators includes simplifying a modeling an output force of a stimuli sensitive actuator in response to stimuli as a linear equation.
5 . The computer-implemented method of claim 1 , wherein the receiving an initial design domain for the truss structure includes receiving at least one of boundary conditions, and loading conditions; and
wherein the producing the design workflow to generate one or more designs with placement of actuators includes producing the design workflow for a one or more portions based on the at least one of boundary conditions and loading conditions.
6 . The computer-implemented method of claim 1 , wherein the producing the design workflow to generate one or more designs includes producing the design workflow to specify members of the truss structure without actuators are fabricated at a first manufacturing location and the design workflow to specify members of the truss structure with actuators that change their shape in response to stimuli are fabricated in a second manufacturing location, and the truss structure is assembled at the second manufacturing location, wherein the first manufacturing location and the second manufacturing location are geographically different.
7 . The computer-implemented method of claim 1 , wherein the simulated fault on the truss structure further comprises:
receiving one or more simulated faults; and
evaluating the one or more designs produced by the design workflow to identify a design that the neutralize at least a portion of the effects of the one or more simulated faults on the truss structure.
8 . The computer-implemented method of claim 1 , wherein the producing the design workflow to generate one or more designs to use additive manufacturing to form one or more of the actuators.
9 . The computer-implemented method of claim 1 , wherein the producing the design workflow to generate one or more designs includes producing the design workflow to specify members of the truss structure with actuators that change their shape in response to stimuli are fabricated at a first manufacturing location and to specify members of the truss structure without actuators are fabricated in a second manufacturing location, wherein the first manufacturing location and the second manufacturing location are geographically different.
10 . The computer-implemented method of claim 1 , wherein the producing the design workflow to generate one or more designs includes producing the design workflow to specify two or more distinct manufacturing locations for fabricating at least two of the plurality of members of the truss structure and assembling these fabricated truss members in a third location to form the truss structure, wherein the distinct manufacturing locations and the third location are each geographically different.
11 . An information processing system for placing sensors on an active resilient structure design, the information processing system comprising:
a computer memory capable of storing machine instructions; and
a hardware processor in communication with the computer memory, the hardware processor configured to access the computer memory to execute the machine instructions to perform
receiving an initial design domain for a truss structure formed from a plurality of members connected by nodes, the members include passive structures and structures formed with stimuli sensitive actuators;
creating a mathematical array of sensor placement sensitivity by successively measuring, for each respective sensor disposed on a respective member of a plurality of members comprising the truss structure, a respective relative change in structural response based on applying respective faults on other members of the plurality of members other than the respective member;
iteratively using the mathematical array of sensor placement sensitivity to evaluate different locations for groups of sensors disposed on the plurality of members in the truss structure, to measure a change in the structural response until at least one of i) a predefined number of stimuli sensitive actuators is reached, ii) a predefined number of sensors is reached, iii) a predefined computational budget is reached, and iv) a predefined computational performance is reached;
identifying, based on the evaluation of different locations of each sensor, locations of a fewest number of sensors in the groups of sensors that produce a relatively larger measured change in the structural response for a given location of a fault; and
producing a design workflow to generate one or more active resilient structure designs based on the locations of the fewest number of sensors that produce the relatively larger measured change in the structural response, in order to neutralize the effects of a simulated fault on the truss structure.
12 . The system of claim 11 , wherein the receiving the initial design domain for a truss structure includes receiving the initial design with at least one of 1) boundary conditions and ii) loading conditions.
13 . The system of claim 11 , wherein the producing the design workflow to generate one or more designs of with placement of stimuli sensitive actuators includes at least one of i) actuators that change their shape in response to stimuli, ii) passive material that does not change its shape in response to stimuli, and iii) materials that have one or more voids.
14 . The system of claim 11 , wherein the producing the design workflow to generate one or more designs of with placement of stimuli sensitive actuators includes simplifying a modeling an output force of a stimuli sensitive actuator in response to stimuli as a linear equation.
15 . The system of claim 11 , wherein the receiving an initial design domain for the truss structure includes receiving at least one of boundary conditions and loading conditions; and
wherein the producing the design workflow to generate one or more designs with placement of actuators includes producing the design workflow for a one or more portions based on the at least one of more boundary conditions and loading conditions.
16 . The system of claim 11 , wherein the producing the design workflow to generate one or more designs includes producing the design workflow to specify members of the truss structure without actuators are fabricated at a first manufacturing location and the design workflow to specify members of the truss structure with actuators that change their shape in response to stimuli are fabricated in a second manufacturing location, and the truss structure is assembled at the second manufacturing location, wherein the first manufacturing location and the second manufacturing location are geographically different.
17 . The system of claim 11 , wherein the simulated fault on the truss structure further comprises:
receiving one or more simulated faults; and
evaluating the one or more designs produced by the design workflow to identify a design that the neutralize at least a portion of the effects of the one or more simulated faults on the truss structure.
18 . The system of claim 11 , wherein the producing the design workflow to generate one or more designs to use additive manufacturing to form one or more of the actuators.
19 . The system of claim 11 , wherein the producing the design workflow to generate one or more designs includes producing the design workflow to specify members of the truss structure with actuators that change their shape in response to stimuli are fabricated at a first manufacturing location and to specify members of the truss structure without actuators are fabricated in a second manufacturing location, wherein the first manufacturing location and the second manufacturing location are geographically different.
20 . The system of claim 11 , wherein the producing the design workflow to generate one or more designs includes producing the design workflow to specify two or more distinct manufacturing locations for fabricating at least two of the plurality of members of the truss structure and assembling these fabricated truss members in a third location to form the truss structure, wherein the distinct manufacturing locations and the third location are each geographically different.