A Model-Based Prognostic Framework for Electromechanical Actuators Based on Metaheuristic Algorithms
Abstract
:1. Introduction
2. Related Work
3. Materials and Methods
- : Dry friction. When , the resulting friction is the nominal value multiplied by three.
- : Backlash. When , the backlash magnitude is the nominal value multiplied by one hundred.
- , , : Short circuit (SC). Being a three-phase motor, each coefficient is linked to a short circuit in one phase.
- , : Static eccentricity. These coefficients are linked to the modulus and phase of the eccentricity in the rotor. Under nominal conditions, the phase corresponds to 0 rad, so .
- : Proportional gain drift (PGD). is linked to an increase of 50 per cent in the proportional gain, while determines a 50 per cent decrease. The nominal value is .
3.1. Employed Algorithms
- PSO, since it resulted as one of the most used ones;
- DE, to represent the evolutionary algorithm category;
- GWO, which we selected among new algorithms.
3.1.1. Evolutionary Algorithms
- Population: The solution “pool”, which is initialized at the start of the process;
- Variety: The population must be varied enough to explore the solution space effectively;
- Heredity: This values is linked to the capability of passing a characteristic to the offspring;
- Selection: For artificial algorithms, selection must only occur in the desired direction, which is a key parameter to ensure that only the best solutions will be reproduced.
3.1.2. Swarm Intelligence Methods
3.2. Models
- Controller: This block is essentially composed of a PID controller. In fact, even if there are much more advanced and sophisticated control logics (e.g., [53]), PID controllers are still the way to go and they are still chosen even in complex systems, as they are easy to implement and tune. PID controllers are composed of three separated branches, where the proportional, differential, and integral action are calculated. The controller aim is comparing the command signals with the actual signal obtained from the motor transmission dynamics block, hence closing the control loop. In this particular case, both position and speed can be monitored. This block outputs the reference current , obtained from the motor torque thanks to the torque constant, which is finally passed to the inverter.
- Inverter: This block contains Clarke-Park equations, and it provides the motor block with the three voltages (one for each phase) for the PMSM motor by performing the corresponding pulse width modulation (PWM). A very complicated physics-based process is handled by Simscape, a specific Simulink library, capable of providing electrical simulation packages. The main actions inside this block are the calculation of the electrical angle starting from the motor position, the splitting of into the three phase currents (with Clarke-Park equations), the PWM process, and the calculation of the three phase voltages, using the fed-back currents.
- Sinusoidal BLDC motor: This block is able to simulate the electrical and magnetic interactions inside a PMSM. It contains Simscape elements, and it manages three main processes:
- The calculation of the counter-electromotive force coefficient for each phase. This is achieved with the multiplication of the back EMF coefficients (obtained with experimental test campaigns) with three sine waves out of phase from each other.
- The implementation of the motor resitive-inductive circuit. A set of mathematical equations (Equation (5)) that model the three star connected LR branches is solved and phase currents () are, hence, calculated. The resistance and inductance of the motor are taken from equipment data sheets.
- The calculation of the motor available torque. Three different electromotive coefficients are used to calculate the motor torque along with the relative phase currents:
- Motor transmission dynamics: this final block compares the available torque with the external requested torque and solves a second-order dynamical system (Equation (7) comprehensive of multiple non linearities, such as dry friction and backlash [52]). The outputs of this block are the motor position and speed, which are looped back to the controller.
4. Results
5. Discussion
6. Conclusions
Author Contributions
Funding
Data Availability Statement
Conflicts of Interest
Abbreviations
MEA | More Electric Aircraft |
EMA | Electro-Mechanical Actuator |
PHM | Prognostic and Health Management |
PMSM | Permanent Magnet Syncrhonous Motor |
DE | Differential Evolution |
PSO | Particle Swarm Optimization |
GWO | Grey Wolf Optimization |
NTB | Numerical Test Bench |
LCC | Life Cycle Costs |
EHA | Electro-Hydraulic Actuators |
CBM | Condition-Based Maintenance |
RAMS | Reliability, Availability, Maintenability, and Safety |
TLBO | Teaching–Learning-Based Optimization |
HGS | Hunger Game Search |
VNS | Variable Neighbourhood Search |
ACO | Ant Colony Optimization |
CSO | Cuckoo Search Optimization |
MM | Monitoring Model |
RM | Reference Model |
SC | Short Circuit |
FDI | Failure Detection and Identification |
ConOps | Concept of Operation |
TLP | Top Level Parameter |
MSA | Metaheuristic Search Algorithm |
EA | Evolutionary Algorithm |
SI | Swarm Intelligence |
GA | Genetic Algorithm |
BLDC | BrushLess Direct Current |
PID | Proportional Integral Derivative |
PWM | Pulse Width Modulation |
FMECA | Failure Mode Effect and Criticality Analysis |
PC | Performance Coefficient |
PHMC | Prognostic and Health Management Computer |
EMF | Electro-Motive Force |
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TLP | Physical Failure | Effect at | Effect at |
---|---|---|---|
Dry friction | No effect (Nominal friction) | of nominal friction | |
Backlash | No effect (Nominal backlash) | 100 times nominal backlash | |
Short circuit (Phase A) | No effect (No SC on Phase A) | Complete SC on phase A | |
Short circuit (Phase B) | No effect (No SC on phase B) | Complete SC on phase B | |
Short circuit (Phase C) | No effect (No SC on phase C) | Complete SC on phase C | |
Eccentricity modulus | No effect (No eccentricity) | Maximum Eccentricity | |
Eccentricity phase | |||
PGD | of nominal proportional gain | of nominal proportional gain |
Characteristic | Value |
---|---|
Rated speed (100 K) | 2000 rpm |
Number of poles | 8 |
Rated torque (100 K) | 5.3 Nm |
Rated current | 3.0 A |
Static torque (60 K) | 5.00 Nm |
Static torque (100 K) | 6.0 Nm |
Stall current (60 K) | 2.55 A |
Stall current (100 K) | 3.15 A |
Efficiency | 90.00 |
Failures | DE | PSO | GWO | ||||||
---|---|---|---|---|---|---|---|---|---|
Time (s) | Err. (%) | PC (%) | Time (s) | Err. (%) | PC (%) | Time (s) | Err. (%) | PC (%) | |
Friction | 3015 | 1.30 | 56.97 | 1342.5 | 1.30 | 80.76 | 2865.5 | 1.20 | 62.26 |
Backlash | 2895 | 1.45 | 50.21 | 980.5 | 1.18 | 86.28 | 2378 | 1.28 | 63.49 |
Short Circuit | 2925.5 | 3.08 | 52.32 | 1566 | 2.64 | 78.12 | 2709 | 2.13 | 69.54 |
Eccentricity | 2995.5 | 2.46 | 62.30 | 2202 | 2.45 | 72.45 | 2479.5 | 2.75 | 65.24 |
Prop. Gain | 2853 | 6.54 | 58.61 | 1403 | 6.38 | 80.14 | 2721.5 | 6.42 | 61.24 |
Total | 2936.8 | 2.96 | 56.75 | 1498.8 | 2.79 | 79.24 | 2530.7 | 2.75 | 64.00 |
Time (s) | Err. (%) | PC (%) | |
---|---|---|---|
DE | 1777.0 | 4.21 | 60.95 |
PSO | 1131.4 | 3.37 | 80.09 |
GWO | 1816.6 | 4.33 | 58.94 |
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Baldo, L.; Querques, I.; Dalla Vedova, M.D.L.; Maggiore, P. A Model-Based Prognostic Framework for Electromechanical Actuators Based on Metaheuristic Algorithms. Aerospace 2023, 10, 293. https://doi.org/10.3390/aerospace10030293
Baldo L, Querques I, Dalla Vedova MDL, Maggiore P. A Model-Based Prognostic Framework for Electromechanical Actuators Based on Metaheuristic Algorithms. Aerospace. 2023; 10(3):293. https://doi.org/10.3390/aerospace10030293
Chicago/Turabian StyleBaldo, Leonardo, Ivana Querques, Matteo Davide Lorenzo Dalla Vedova, and Paolo Maggiore. 2023. "A Model-Based Prognostic Framework for Electromechanical Actuators Based on Metaheuristic Algorithms" Aerospace 10, no. 3: 293. https://doi.org/10.3390/aerospace10030293
APA StyleBaldo, L., Querques, I., Dalla Vedova, M. D. L., & Maggiore, P. (2023). A Model-Based Prognostic Framework for Electromechanical Actuators Based on Metaheuristic Algorithms. Aerospace, 10(3), 293. https://doi.org/10.3390/aerospace10030293