Introduction to Mechatronics Systems

Chapter 11
System Integration, Prototyping and Verification

Bachelor Program in Mechatronics Engineering
Introduction to Mechatronics Systems   •   Bachelor

System Integration, Prototyping and Verification

Introduction

A mechatronic system is not merely a collection of mechanical, electrical, software, and control components. Its useful behavior emerges from the interaction of these components through physical, electrical, informational, and human interfaces. System integration is the disciplined process of combining subsystems into a functioning whole and demonstrating that the whole satisfies its requirements.

Integration is often where weaknesses in earlier design decisions become visible. A motor may meet its torque specification when tested alone but fail when connected to a mechanism. A sensor may be accurate on a workbench but produce unreliable readings near a switching power converter. A controller may perform well in simulation but become unstable when sampling delays, actuator saturation, communication losses, and mechanical backlash are introduced.

This chapter presents a practical framework for building, integrating, verifying, validating, troubleshooting, and documenting a mechatronic prototype. The discussion applies to systems such as robotic manipulators, automated production equipment, autonomous vehicles, medical devices, smart appliances, and laboratory platforms.

Learning Objectives

After studying this chapter, the reader should be able to:

  1. Explain the purpose and stages of mechatronic system integration.
  2. Define and manage interfaces between mechanical, electrical, software, and control subsystems.
  3. Plan a prototype using staged integration and appropriate test evidence.
  4. Distinguish verification from validation and select suitable tests for each.
  5. Apply hardware-in-the-loop testing to reduce integration risk.
  6. Diagnose faults using structured troubleshooting methods.
  7. Evaluate performance using measurable technical criteria.
  8. Produce professional integration, test, configuration, and safety documentation.
  9. Assess a complete prototype against requirements and identify remaining limitations.

1. Integration as a Systems Engineering Activity

1.1 From subsystem design to system behavior

Subsystem design usually focuses on local objectives: a mechanical assembly must carry a load, a motor drive must regulate current, a sensor must provide a signal, and software must execute an algorithm. Integration addresses system-level questions:

  • Do the subsystems use compatible voltage, current, timing, and communication conventions?
  • Are coordinate systems and units consistent?
  • Does the actuator have adequate authority under the real load?
  • Can the controller respond within the available sampling and communication delays?
  • What happens when a sensor fails or a communication message is lost?
  • Can an operator safely start, stop, inspect, and maintain the system?

A system requirement should be traceable to one or more design elements and to objective verification evidence. A useful traceability chain is:

Requirement → design feature → implementation → test procedure → test result.

Without this chain, a prototype may appear functional while important requirements remain untested.

1.2 The integration hierarchy

Integration is normally performed from lower-risk interfaces to higher-risk system functions. A typical hierarchy is:

  1. Component testing: individual sensors, actuators, boards, mechanisms, and software modules.
  2. Subsystem testing: for example, motor plus drive plus encoder, or sensor plus signal-conditioning circuit.
  3. Interface testing: electrical, mechanical, communication, timing, and software interfaces.
  4. Functional integration: closed-loop operation under controlled conditions.
  5. System-level testing: complete operation in the intended environment.
  6. Acceptance and validation: evidence that the system solves the intended user or operational problem.

The hierarchy should not be interpreted as a rigid one-way sequence. Iteration is expected. However, uncontrolled “big-bang” integration—connecting everything at once—makes fault isolation difficult because many variables change simultaneously.

Staged mechatronic system integration flow Componentsunit tests Subsystemsbench tests Interfacescompatibility Integratedclosed loop Validated systemreal context Increasing interaction and operational realism At each stage: define configuration, test safely, record evidence, and review defects.
Staged mechatronic system integration flow
Figure: Staged mechatronic system integration flow

Figure: Staged integration reduces diagnostic ambiguity while progressively increasing system realism.

2. Interface Management

An interface is a defined boundary across which energy, matter, information, structure, or control authority passes. Interface management makes these boundaries explicit rather than leaving compatibility to assumption.

2.1 Types of interfaces

Interface typeTypical parametersExample failure
Mechanicaldimensions, tolerances, loads, stiffness, alignmentshaft coupling binds
Electrical powervoltage, current, grounding, protection, connectorscontroller resets during acceleration
Electrical signallogic levels, polarity, isolation, bandwidthsensor output is overvoltage
Communicationprotocol, address, baud rate, message format, timingincorrect byte order
Softwaredata types, units, states, error codes, APIsradians interpreted as degrees
Temporalsample period, latency, synchronization, deadlinesstale feedback destabilizes control
Human/operatordisplays, controls, warnings, access, trainingunsafe restart after a fault
Environmentaltemperature, vibration, dust, electromagnetic interferenceintermittent sensor readings

An interface control document (ICD) records the agreed characteristics of each important interface. An effective ICD includes the interface name, responsible owners, physical connection, signal or data definition, units, limits, timing, safety constraints, verification method, and revision history.

2.2 Units, coordinate systems, and data conventions

Many integration failures are semantic rather than physical. Every measurement should have an explicit unit and, where applicable, a reference frame and sign convention. For example, a position message should specify whether it is measured in millimetres or metres, whether positive motion is clockwise or counterclockwise, and whether the angle is expressed in degrees or radians.

A coordinate transformation may be required between a sensor frame and a mechanism frame. For a planar rotation and translation, a point can be represented using a homogeneous transformation matrix:

pA = TAB pB

where pB is a point expressed in frame B, pA is the same point expressed in frame A, and TAB is the 3 × 3 transformation matrix. The transformation is valid only when the frame definitions and multiplication order are consistent. In three-dimensional robotics, 4 × 4 homogeneous transformations are commonly used.

2.3 Interface risk

Interfaces deserve early attention because they couple otherwise acceptable subsystems. A simple risk score can prioritize work:

R = S × O × D

where S is severity, O is occurrence likelihood, and D is difficulty of detecting the failure before harm or defect escape. The numerical scales must be defined by the project; the product is a prioritization aid, not a probability law. High-risk interfaces should receive early tests, protective design, and explicit review.

3. Prototyping Strategy

3.1 Purpose of a prototype

A prototype is an experimental system built to obtain evidence. It may demonstrate technical feasibility, expose interface problems, estimate performance, support user evaluation, or prepare a production design. A prototype should therefore have a stated purpose and success criteria. A visually impressive assembly is not necessarily a useful prototype if it cannot produce reliable evidence.

Prototypes can be classified as:

  • Proof-of-principle prototypes, which test whether a concept can work.
  • Breadboard prototypes, which expose connections and support rapid modification.
  • Engineering prototypes, which integrate representative hardware and software.
  • Appearance or ergonomic prototypes, which assess user interaction and physical form.
  • Pre-production prototypes, which approximate manufacturing and operational conditions.

3.2 Incremental integration

A robust prototype plan identifies integration increments. For example, an automated positioning axis may be integrated in this order:

  1. Inspect wiring, fasteners, grounding, and mechanical travel.
  2. Verify emergency stop and power-disconnect functions.
  3. Operate the drive with the mechanism unloaded at low speed.
  4. Confirm encoder direction and position scaling.
  5. Run open-loop or limited-motion tests with physical restraints.
  6. Close the position loop with conservative gains.
  7. Add the production payload and evaluate temperature, vibration, and tracking error.
  8. Test abnormal conditions, recovery, and operator procedures.

Each increment should have entry criteria, a controlled procedure, expected results, exit criteria, and a rollback plan.

3.3 Prototype fidelity

A model is useful only if it reproduces the phenomena relevant to the question being investigated. A low-fidelity model may be sufficient for control logic, whereas actuator thermal behavior requires representative electrical resistance, current, duty cycle, and heat dissipation. Hardware should be substituted for simulation when uncertainty in that hardware dominates the risk.

4. Verification and Validation

Verification asks: “Was the system built according to its specified requirements?” Validation asks: “Does the system meet the intended need in its operational context?” A system can be verified but not validated—for example, a robot may meet its programmed accuracy specification but be too slow or difficult for the operator’s workflow.

4.1 The V-model perspective

The left side of a systems engineering V-model decomposes user needs into system requirements, subsystem requirements, and detailed designs. The right side integrates and tests in the reverse direction. Unit tests correspond to detailed design, subsystem tests correspond to subsystem requirements, system verification corresponds to system requirements, and validation corresponds to operational need.

4.2 Verification methods

Four common methods are:

  • Inspection: visual or document examination, such as confirming connector labeling.
  • Analysis: calculation, simulation, or review of evidence, such as estimating structural stress.
  • Demonstration: observing operation under specified conditions.
  • Test: measuring a response using controlled equipment and defined acceptance limits.

A requirement should use measurable language. “The carriage shall move quickly” is weak. “The carriage shall travel 500 mm in no more than 4 s while carrying 2 kg” is testable, provided the acceleration profile and measurement method are defined.

4.3 Measurement and performance metrics

For a measured quantity yi and a reference value ri, the error is:

ei = yi − ri

The mean absolute error over N observations is:

MAE = (1/N) ∑i=1N |ei|

The root-mean-square error is:

RMSE = √[(1/N) ∑i=1N ei²]

Both metrics have the same units as the measured variable. MAE gives an average magnitude of error, while RMSE weights larger errors more strongly. They summarize performance but do not replace examination of time histories, overshoot, settling time, saturation, or failure events.

For a step response, percent overshoot can be defined as:

Mp = [(ymax − y_∞)/|y_∞ − y0|] × 100%

where ymax is the maximum response, y_∞ is the final value, and y0 is the initial value. This expression assumes a nonzero step and a response for which a meaningful final value exists.

A measured value should be reported with measurement uncertainty when it affects a decision. If independent uncertainty sources are combined using a root-sum-square estimate, then:

uc = √(u1² + u2² + … + uk²)

where uj are standard uncertainties. This approximation assumes the sources are independent and approximately linear in the measured result; correlated or strongly nonlinear effects require a more careful uncertainty analysis.

4.4 Test design

A test specification should state:

  • requirement identifier and purpose;
  • equipment, calibration status, and software version;
  • physical configuration and environmental conditions;
  • input profile and initial state;
  • measured variables and sampling rate;
  • safety controls and abort conditions;
  • acceptance criteria;
  • raw data location and analyst;
  • result, deviations, and disposition.

Repeatability concerns variation when the same method, equipment, operator, and conditions are used. Reproducibility concerns variation when relevant conditions, operators, or equipment change. Both matter when a prototype is expected to operate beyond its development laboratory.

5. Hardware-in-the-Loop Testing

Hardware-in-the-loop (HIL) testing connects real hardware—such as a controller, motor drive, or sensor interface—to a real-time simulation of the remaining system. The simulator must execute each model step before the next real-time deadline. HIL is valuable when full-system tests are expensive, dangerous, slow, or difficult to repeat.

Examples include:

  • connecting an actual flight controller to a simulated vehicle;
  • connecting a motor controller to a real-time motor and load model;
  • testing an automotive electronic control unit against simulated vehicle dynamics;
  • injecting simulated sensor faults into a real control computer.

A HIL model is not automatically accurate. Its validity depends on the phenomena included, numerical step size, interface latency, signal scaling, and real-time performance. A useful HIL campaign compares selected HIL outputs with analytical calculations, offline simulation, and physical experiments.

Important HIL tests include nominal operation, sensor bias, noise, quantization, actuator saturation, communication delay, dropped packets, power-up sequencing, and emergency shutdown. Fault injection should be controlled and documented; it must not create uncontrolled hazards.

6. Control and Timing During Integration

Closed-loop behavior depends on the complete loop, not only on the controller equation. Sensor filtering, sample-and-hold behavior, computation time, communication delay, actuator dynamics, and mechanical compliance all contribute phase lag and can reduce stability margins.

For a digital controller, the sample period is:

Ts = 1/fs

where Ts is the sampling period in seconds and fs is the sampling frequency in hertz. This relationship is a definition and assumes a regular sampling schedule. In practice, jitter means that the actual interval varies around the nominal value; that variation should be measured when timing is safety- or stability-critical.

A proportional-integral-derivative controller is often written:

u(t) = Kp e(t) + Ki ∫₀ᵗ e(τ)dτ + Kd de(t)/dt

where e(t) is the error, u(t) is the command, and Kp, Ki, and Kd are controller gains. This ideal form assumes a continuous signal and an available derivative. Real implementations usually filter the derivative, limit the command, and prevent integrator windup. The equation alone does not guarantee stability; stability depends on the plant, sampling, delays, gains, saturation, and implementation.

During integration, record command, feedback, error, controller output, saturation status, timestamps, and relevant fault states. These signals often reveal whether poor performance is caused by incorrect scaling, mechanical friction, insufficient authority, timing problems, or tuning.

7. Structured Troubleshooting

Troubleshooting should be an evidence-based process rather than random adjustment. A practical sequence is:

  1. Make the system safe and preserve the original configuration.
  2. Describe the symptom precisely: when it occurs, under what conditions, and how often.
  3. Check recent changes and configuration versions.
  4. Divide the system at an interface and test from known-good boundaries.
  5. Measure power, signals, timing, and state transitions.
  6. Form competing hypotheses and design tests that distinguish them.
  7. Change one relevant variable at a time.
  8. Record the finding, corrective action, and regression test.

The “five whys” method can help identify contributing causes, but it should not be used to force a single simplistic root cause. Fault trees are useful for showing how combinations of events lead to a hazardous top event. A fishbone diagram can organize possible causes under categories such as mechanical, electrical, software, measurement, environment, and human factors.

Common integration faults include:

  • reversed encoder direction;
  • incorrect unit conversion;
  • missing common reference or improper grounding;
  • voltage drop during transient loads;
  • connector pin mismatch;
  • race conditions and stale messages;
  • excessive backlash or compliance;
  • integrator windup;
  • unhandled startup or shutdown states;
  • electromagnetic interference;
  • thermal overload;
  • safety interlocks bypassed during debugging.

A fault log should contain a unique identifier, date, configuration, symptom, severity, suspected cause, evidence, action, owner, status, and regression-test reference.

8. Safety, Ethics, and Governance

A prototype is not exempt from engineering responsibility because it is experimental. Risk assessment should consider hazards from motion, stored energy, electrical shock, heat, pressure, sharp edges, software malfunction, unexpected restart, and loss of communication. Controls should follow a hierarchy: eliminate the hazard where possible, reduce risk by design, add guarding and interlocks, provide warnings and procedures, and use personal protective equipment as a final layer.

Emergency stops should place the system in a defined safe state. The safe state is application-dependent: removing motor torque may be appropriate for a robot, whereas an abrupt stop may be unsafe for a cutting process or suspended load. Restart behavior must be deliberate and should not occur merely because a transient fault disappears.

Engineers must also consider cybersecurity, privacy, accessibility, and misuse. A connected prototype may expose control interfaces or collect operator data. Access control, secure update procedures, logging, and least-privilege design are appropriate where communication networks are involved. AI-based perception or decision functions require additional evaluation of dataset limitations, false detections, explainability, human oversight, and safe fallback behavior. AI should not be treated as evidence of correctness; its outputs must be verified against defined performance and safety requirements.

Applicable standards depend on the sector and jurisdiction. Examples may include machinery safety, functional safety, electromagnetic compatibility, electrical safety, robotics, medical devices, or automotive regulations. Standards should be identified early because they influence architecture, test evidence, documentation, and change control.

9. Documentation and Configuration Control

Professional integration depends on controlled information. The minimum documentation set commonly includes:

  • system architecture and block diagrams;
  • requirements and verification traceability matrix;
  • interface control documents;
  • schematics, drawings, bills of materials, and wiring schedules;
  • software source, build instructions, and configuration files;
  • calibration records;
  • risk assessment and safety procedures;
  • test plans, raw data, scripts, plots, and reports;
  • fault and change logs;
  • operating, maintenance, and training instructions.

Configuration control identifies exactly what was tested. Hardware revision, firmware version, software commit, parameter set, calibration file, and test-equipment status should be recorded. A test result without configuration identity is difficult to reproduce and weak as engineering evidence.

Change control does not mean preventing all changes. It means assessing the effect of a change, approving it at an appropriate level, updating affected documents, and repeating necessary verification. Baselines should be established before formal demonstrations or acceptance tests.

10. Worked Example: Verification of a Positioning Axis

An illustrative prototype uses a belt-driven linear axis. The requirement is that, with a 1.5 kg payload, the axis shall move 400 mm and settle within ±0.50 mm of the commanded position within 2.0 s. Three repeated tests produce final position errors of +0.20 mm, −0.35 mm, and +0.10 mm.

The absolute errors are 0.20 mm, 0.35 mm, and 0.10 mm. Therefore:

MAE = (0.20 + 0.35 + 0.10)/3 = 0.2167 mm ≈ 0.22 mm

The RMSE is:

RMSE = √[(0.20² + 0.35² + 0.10²)/3]
= √(0.1725/3) mm
= √0.0575 mm
≈ 0.24 mm

Both summary metrics are below 0.50 mm, but the requirement must also be checked test by test. The largest absolute error is 0.35 mm, so all three final errors satisfy the stated tolerance. If one test had an error of 0.70 mm, a low average could not conceal the individual requirement failure. The engineer should then examine the time trace, payload alignment, belt tension, drive current, and encoder data rather than merely retuning the controller.

11. Illustrative Case: Automated Pick-and-Place Prototype

Background

A university-industry project develops a two-axis pick-and-place unit for sorting small packages. The system includes a frame, belt-driven axes, stepper motors, optical presence sensors, a camera, a microcontroller, a supervisory computer, and a pneumatic gripper.

Problem

Initial assembly succeeds in moving the axes, but the complete system occasionally misses packages and sometimes restarts when both axes accelerate. The team initially suspects the vision algorithm.

Analysis

The integration team creates an interface matrix and records voltage, current, timestamps, sensor states, motor commands, and software faults. The results show two distinct problems. First, the camera coordinate origin is offset from the mechanical coordinate origin by a fixed translation. Second, the 24 V supply drops below the controller’s allowed input range during simultaneous acceleration. The pneumatic valve also produces electrical noise when it switches.

Approach and solution

The team first separates the faults using staged tests. A calibration procedure estimates the camera-to-table transformation using known reference points. The transformation is stored with a calibration identifier and checked after mechanical disturbance. For the power problem, the team measures the supply at the controller terminals rather than only at the power supply. It then separates high-current motor wiring, improves return paths, adds suitable suppression at the valve interface, and introduces a controlled acceleration profile. A power-on sequence prevents motion commands until sensors and communication links report valid states.

HIL testing is used before repeating full-speed physical trials. Simulated package positions and delayed sensor messages test the supervisory state machine. Fault injection confirms that a missing camera message produces a safe stop and a diagnostic code rather than an uncontrolled movement.

Outcome

The prototype achieves the sorting sequence under the defined payload and speed conditions. Verification evidence includes coordinate-calibration results, voltage transients, cycle-time measurements, missed-pick counts, emergency-stop tests, and software version records. Validation with operators reveals an additional issue: the reset control is difficult to reach while loading packages. The control panel is relocated and its status indication is improved.

Learning points

The case demonstrates that apparent algorithmic failures may originate in coordinate conventions, power integrity, timing, or human-machine interaction. It also shows why validation cannot be replaced by laboratory verification: the operators identified a usability and access problem that component tests could not reveal.

12. Contemporary Developments and Best Practices

Digital twins increasingly combine physical prototypes, real-time data, and models. Their value depends on model credibility, sensor quality, synchronization, and clearly stated limits. Automated test frameworks can execute regression tests after software changes, but automation must include meaningful assertions and inspection of anomalous results. Continuous integration is particularly useful for embedded software, parameter checking, communication protocols, and simulation-based tests.

Modern systems also use condition monitoring, edge computing, wireless communication, and machine learning. These technologies increase capability but introduce additional interfaces, attack surfaces, latency, data-quality problems, and maintenance requirements. A disciplined integration process remains essential.

Best practices include:

  • define measurable requirements before building;
  • identify high-risk interfaces early;
  • integrate in small, reversible increments;
  • use representative loads and environmental conditions;
  • record raw data, not only pass/fail conclusions;
  • distinguish verification from validation;
  • test abnormal behavior and recovery;
  • maintain configuration and calibration control;
  • protect people before protecting schedules;
  • perform regression tests after every significant change;
  • communicate limitations honestly to users and decision-makers.

Chapter Summary

System integration combines mechanical, electrical, software, control, human, and environmental elements into a functioning mechatronic system. Successful integration requires explicit interface definitions, consistent units and coordinate frames, staged prototyping, controlled configuration, and evidence-based troubleshooting. Verification demonstrates conformity with specified requirements, whereas validation demonstrates suitability for the intended operational need. HIL testing provides repeatable evaluation of real controllers and interfaces before complete physical testing, but its models and timing must be credible. Performance should be evaluated with appropriate metrics, time histories, uncertainty considerations, and requirement-level acceptance criteria. Safety, cybersecurity, documentation, calibration, and change control are integral engineering responsibilities. A professional prototype is therefore not simply one that operates; it is one whose behavior, limitations, risks, and evidence are understood and traceable.

Key Terms

System integration: Combining subsystems and interfaces into a functioning complete system.

Prototype: An experimental implementation built to obtain evidence about a design.

Interface: A defined boundary across which energy, information, structure, or control passes.

Interface control document: A controlled record specifying the characteristics and responsibilities of an interface.

Verification: Demonstration that specified requirements have been satisfied.

Validation: Demonstration that the system meets its intended operational need.

Traceability: The documented connection between requirements, design, implementation, and evidence.

Hardware-in-the-loop: Testing real hardware with a real-time simulation of other system elements.

Configuration control: Management of revisions so that tested system states are identifiable and reproducible.

Acceptance criterion: A defined condition used to decide whether a test result passes.

Regression test: A repeated test used to detect defects introduced by changes.

Sampling period: Time between successive digital measurements or control updates.

Latency: Delay between an event, its measurement, processing, and resulting action.

Actuator saturation: Operation in which an actuator reaches its physical or command limit.

Fault injection: Deliberate introduction of a defined fault to assess detection and response.

Root cause: An underlying condition whose removal prevents recurrence of a problem.

Calibration: Establishing the relationship between measurement output and a reference.

Risk assessment: Structured evaluation of hazards, likelihood, severity, and controls.

Mean absolute error: Average magnitude of measurement or tracking errors.

Configuration baseline: An approved, identified system state used as a reference for testing or release.

Review Questions

Short Answer Questions

  1. What is the difference between verification and validation?
  2. Why are interface control documents useful during system integration?
  3. Name four common methods of verification.
  4. What information should be recorded in a test specification?
  5. Why should integration normally proceed in stages rather than by a single big-bang assembly?

Long Answer Questions

  1. Explain how mechanical, electrical, communication, software, and temporal interfaces can interact to produce system-level failures.
  2. Describe a complete staged integration plan for a closed-loop mechatronic axis.
  3. Explain the purpose, benefits, and limitations of hardware-in-the-loop testing.
  4. Discuss how configuration control and traceability improve the credibility of prototype test results.
  5. Develop a safety and documentation strategy for an automated machine prototype.

Analytical / Application Questions

  1. A position-control prototype has a low average error but one large error during acceleration. Explain why the average alone is insufficient and propose additional tests.
  2. A controller resets whenever two motors start simultaneously. Develop a troubleshooting plan that distinguishes power integrity, grounding, software, and electromagnetic-interference causes.
  3. Design a verification and validation matrix for a camera-guided pick-and-place system, including requirements, test methods, measurements, and acceptance evidence.

Multiple Choice Questions with Answers

Question 1

Which statement best distinguishes verification from validation?

A. Verification tests whether requirements were met; validation tests whether the intended need was met.

B. Verification is performed only with software; validation is performed only with hardware.

C. Verification occurs after validation and does not require measurable requirements.

D. Verification concerns safety only; validation concerns cost only.

Correct Answer: A. Verification tests whether requirements were met; validation tests whether the intended need was met.

Question 2

What is the primary purpose of an interface control document?

A. To replace all system requirements with wiring diagrams

B. To define and control the characteristics and responsibilities of an interface

C. To calculate the theoretical stability of a controller

D. To record only operator training results

Correct Answer: B. To define and control the characteristics and responsibilities of an interface

Question 3

A test produces errors of 0.20 mm, −0.35 mm, and 0.10 mm. What is the approximate MAE?

A. 0.10 mm

B. 0.20 mm

C. 0.22 mm

D. 0.35 mm

Correct Answer: C. 0.22 mm

Question 4

Which is an example of hardware-in-the-loop testing?

A. Testing a CAD drawing without physical or simulated behavior

B. Connecting a real controller to a real-time simulation of the plant

C. Operating a complete machine without recording data

D. Inspecting a connector with the power removed

Correct Answer: B. Connecting a real controller to a real-time simulation of the plant

Question 5

Which metric weights large errors more strongly than MAE?

A. RMSE

B. Sampling period

C. Latency

D. Percent uptime

Correct Answer: A. RMSE

Question 6

What is the most appropriate first response when an integrated prototype behaves unexpectedly?

A. Increase all controller gains immediately

B. Change several hardware and software variables simultaneously

C. Make the system safe and preserve the configuration while describing the symptom

D. Delete the previous test data

Correct Answer: C. Make the system safe and preserve the configuration while describing the symptom

Question 7

If a digital controller operates at 200 Hz, what is its nominal sampling period?

A. 0.5 ms

B. 5 ms

C. 20 ms

D. 200 ms

Correct Answer: B. 5 ms

Question 8

Which item most directly supports reproducibility of a test result?

A. A photograph without a date or configuration identifier

B. A pass/fail statement without raw data

C. The tested hardware revision, software version, parameters, and calibration status

D. An informal verbal report from the operator

Correct Answer: C. The tested hardware revision, software version, parameters, and calibration status

Question 9

Why can a system be verified but not validated?

A. It may meet technical specifications but fail to serve the user’s operational workflow.

B. Verification never uses measurements.

C. Validation is only concerned with component dimensions.

D. A verified system cannot contain software.

Correct Answer: A. It may meet technical specifications but fail to serve the user’s operational workflow.

Question 10

Which action is an example of fault injection?

A. Replacing a requirement with a design preference

B. Deliberately introducing a dropped communication message to test fault handling

C. Increasing the payload without recording it

D. Removing all safety interlocks before testing

Correct Answer: B. Deliberately introducing a dropped communication message to test fault handling

Introduction to Mechatronics Systems
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