Crane R&D Validation Process: Adams, Simulink and HIL Testing

Inside Kelude's Crane R&D Verification: From Adams/Simulink to HIL. For decades, trial-and-error dominated crane development, dragging out timelines and inflating validation costs. Kelude Heavy Industry has replaced that model with a fully integrated verification pipeline spanning Adams/Simulink through HIL testing—slashing time-to-market for new models.

From Trial-and-Error to Simulation: A New Era in Crane Engineering

Kelude Heavy Industry · R&D Verification Workflow
①Requirements
Duty-cycle analysis
②Concept Design
Structural calculation
③Adams Simulation
Multi-body dynamics
④Simulink Modeling
Control system
⑤MIL
Model-in-the-loop
⑥SIL
Software-in-the-loop
⑦HIL
Hardware-in-the-loop
⑧Field Validation
Load testing
Concept design
Co-simulation
X-in-the-Loop verification
Field confirmation

In traditional crane development, the "trial-and-error" approach has long dominated—build a prototype, test it, find defects, then rework and start over. For a large smart crane, prototype manufacturing alone can cost millions of RMB, and a single extreme-condition test (such as full-load emergency braking or off-center lifting) risks equipment damage or even safety incidents. As cranes become increasingly intelligent, control system complexity grows exponentially, rendering traditional methods inadequate.

The Kelude R&D team understands this challenge well and has built a "multi-level simulation verification" development framework at the system level. The core philosophy: complete over 90% of control logic validation and over 90% of extreme-condition simulation before physical manufacturing begins, minimizing risks during the real-machine testing phase and cutting development cycles by more than 40%.

Co-Simulation Platform: Adams + Simulink Architecture

Co-simulation is the cornerstone of Kelude's R&D framework. The platform is powered by two core engines:

Adams (Multi-Body Dynamics Simulation)

Adams (Automatic Dynamic Analysis of Mechanical Systems) builds the crane's mechanical model—including all kinematic joints such as the boom, slewing mechanism, hoisting mechanism, travel mechanism, and wire rope pulley system. By precisely defining mass, inertia, stiffness, and damping parameters for each component, Adams delivers high-fidelity simulation of dynamic responses under complex operating conditions, covering structural elastic deformation, multi-body coupled vibration, and nonlinear contact phenomena. The model also incorporates flexible-body characteristics of wire ropes, realistically simulating pendulum dynamics during hoisting operations.

Simulink (Control System Simulation)

Simulink hosts the crane's control algorithm models—including speed/position closed-loop control for each mechanism, anti-sway control logic, load moment limiter (LML) algorithms, and safety interlock logic. The control logic running in the Simulink model remains strictly consistent with the program ultimately deployed to the actual PLC.

Co-Simulation Interface

Adams and Simulink exchange data bidirectionally in real time through the Co-Simulation interface: Adams transmits real-time states—position, velocity, acceleration, torque—of each mechanism to Simulink, while Simulink returns controller output commands (such as VFD frequency setpoints and brake actuation signals) to Adams. This closed-loop simulation architecture enables R&D engineers to execute the complete verification chain—"sensor sampling → controller computation → actuator response → mechanical system dynamics"—entirely within a virtual environment.

SIL (Software-in-the-Loop) Testing Process

SIL testing serves as the first verification gate above co-simulation. During the SIL phase, control software (not yet deployed to PLC hardware) is compiled into a PC-executable program and run on the same or a networked computing node alongside the Adams/Simulink co-simulation model.

The core value of SIL testing lies in:

  • Control logic correctness verification: Confirming that speed curves, acceleration/deceleration times, and safety interlock conditions for each mechanism align with design specifications
  • Boundary condition testing: Exercising control behavior under all input signal combinations at the software level, covering both normal and abnormal operating sequences
  • Regression testing: Automatically running the SIL test suite after every control software iteration to ensure modifications introduce no new defects

Kelude's team has built a library of over 200 SIL test cases, covering all operating modes and safety functions.

HIL (Hardware-in-the-Loop) Testing: Real PLC + Virtual Plant

HIL testing is the pivotal link in Kelude's R&D framework. Its core architecture:

Real PLC (S7-1500) + Real-Time Simulator (running Adams dynamics model in real time)

In HIL testing:

  1. The device under test is a real S7-1500 PLC running the final version of the control program (identical to the production machine)
  2. The PLC communicates with the real-time simulator via PROFINET/Profinet IO
  3. The simulator runs the Adams dynamics model in real time, feeding virtual sensor signals back to the PLC (angle encoders, load sensors, limit switches, etc.)
  4. PLC outputs (VFD control words, brake signals, etc.) are received by the simulator in real time to drive the virtual mechanical model

The key advantage of this architecture: PLC hardware in the loop, real control program execution, and virtual plant response—all three simultaneously satisfied, enabling comprehensive hardware-level control system verification without requiring a physical crane.

Extreme-Condition Test Coverage

Kelude's R&D verification framework systematically simulates the following extreme operating conditions:

Duty CategoryTestingContentInvolvingStandard
Full-Load Emergency Stop110%rated loadUnder EmergencyBraking,VerificationBrakeThermal Capacity and Structural Impact ResponseISO 4301 Crane Design Standard-2008
Eccentric LoadHoisting / LiftingLoadEccentric Lifting Condition,Verify the Complete MachineAnti-Overturning Stabilityand StructureStrengthISO 4301 Crane Design Standard-2008
WindLoadEccentric Lifting Condition6~12Wind LevelLoadComplete Machine UnderStabilityand Anti-Wind Anti-Slip SafetyISO 4301 Crane Design Standard-2008
earthquakeLoadSeismic Fortification Intensity8Seismic Fortification IntensityearthquakeDynamic Input,Verify Structural Integrity andemergency shutdownSequenceGB/T 25710-2010
Multi-Mechanism LinkageLuffing+Slewing+Hoisting / LiftingCoupled Dynamic Response of Simultaneous ActionsTesting——
SensorFaultAngleencoder disconnection,Load SensorFailureFault Injection, etc.TestingISO 13849-1:2023

Each operating condition generates a detailed simulation test report, including time-domain response curves, spectrum analysis, fatigue damage assessment, and other quantitative data, which serve as the baseline reference for physical machine verification.

From Simulation to Physical Testing: A Closed-Loop Verification Workflow

Kelude's R&D verification system follows a complete "V-shaped" validation workflow:

  1. Requirements Analysis & Simulation Planning – Define test cases and acceptance standards at each level based on design specifications and code requirements.
  2. Model Development & Calibration – Build Adams dynamics models and Simulink control models, then calibrate them using component-level test data.
  3. SIL Verification – Validate control logic at the pure software level.
  4. HIL Verification – Run real-time simulation with PLC hardware-in-the-loop.
  5. Physical Machine Testing – Execute critical operating condition tests on an actual crane and capture real-world measurement data.
  6. Data Feedback & Model Iteration – Feed physical test data back into the simulation models, refine parameters, and improve simulation fidelity.

This closed-loop mechanism allows simulation models to continuously "evolve" as project data accumulates, steadily narrowing the gap between simulation and real-world performance. According to Kelude's internal data, after three or more rounds of model iteration and calibration, the deviation between simulation and physical test results for critical operating conditions has been reduced to within 5%.

R&D Team Structure and Patent Portfolio

Kelude's R&D team is organized around a three-pillar architecture: system-level simulation, control algorithms, and hardware testing.

  • System Simulation Group – Responsible for Adams multi-body dynamics modeling, co-simulation platform maintenance, and design of extreme operating condition test cases.
  • Control Algorithm Group – Handles Simulink control model development, anti-sway algorithms, path planning algorithms, and safety logic design.
  • Test & Validation Group – Manages SIL/HIL test platform setup, test execution, and analysis report preparation.

On the patent front, Kelude has filed multiple invention patents centered on its simulation and verification system, covering core areas such as co-simulation interface methods, HIL test apparatus structures, automatic generation algorithms for extreme-condition test matrices, and closed-loop calibration methods between simulation and physical testing. These patents not only protect the company's technical achievements but also establish a strong moat in the field of smart crane simulation and verification.

It's worth noting that Kelude's R&D verification system is not limited to new product development—it is equally applicable to intelligent retrofit projects for cranes already in service. The key difference is that retrofit projects require reverse modeling based on measured structural parameters of the existing equipment, with particular emphasis on verifying interface compatibility and safety interlock logic between the old and new control systems. For special simulation and verification requirements specific to explosion-proof cranes, please refer to the explosion-proof technology section; for real-world applications of simulation verification in retrofit projects, see the retrofit case studies section.

Economic Benefits and Technical Value of the Verification System

From an economic standpoint, the return on investment for Kelude's R&D verification system is substantial. According to data from the R&D center:

  • Fewer Prototype Iterations – Reduced from an average of 4–5 physical prototype iterations in the traditional model to just 1–2 today, with some mature models achieving "design once, build once, pass once" on the first attempt.
  • Shorter Test Cycles – The complete verification cycle from simulation to physical testing has been compressed from 12–18 months down to 7–10 months.
  • Lower Field Failure Rates – On-site control system failure rates within 12 months of commissioning have dropped by 76% compared to pre-system levels.
  • Higher Certification Pass Rates – The first-attempt pass rate for type tests has improved from 65% to over 92%.

From a technical perspective, the value of this system manifests at three levels. First, it establishes a digital R&D pipeline from virtual simulation to physical hardware, enabling design changes to be validated through simulation within hours rather than waiting weeks for prototype modifications. Second, the vast amount of simulation data lays a solid foundation for future intelligent upgrades of downstream products, such as digital twin implementations and predictive maintenance. Third, the standardized verification process enables efficient knowledge reuse across different projects, significantly shortening the training period for new engineers.

Kelude's R&D verification system has completed three rounds of internal review and technical iteration, and the company is actively pursuing software copyright registrations and technical standard initiatives. Looking ahead, the team plans to extend the verification system into full life cycle management for cranes, including digital twin-based in-service health monitoring, simulation-driven remaining life prediction, and HIL-based remote software upgrade validation.

Frequently Asked Questions (FAQ)

Q: How is real-time performance ensured in Adams/Simulink co-simulation?
A: Co-simulation relies on a fixed-step solver, typically configured with a step size of 1 ms or 0.5 ms. Adams employs stiff integrators such as GSTIFF or WSTIFF, while Simulink uses a discrete solver. On a high-performance simulation workstation, real-time performance at a 1 ms step size can be maintained above 90%. For HIL testing, a dedicated real-time simulator (e.g., dSPACE or NI PXI) runs the Adams model to guarantee hard real-time scheduling.
Q: Can HIL testing fully replace physical machine testing?
A: No, it cannot fully replace physical testing. HIL testing covers the verification of control logic and interface functionality, but it cannot substitute for physical-level validation in real-machine testing, such as structural strength, fatigue life, and electromagnetic compatibility (EMC). The core value of HIL lies in completing the majority of control logic verification before physical testing, significantly reducing the risk and cost of real-machine tests—but it does not eliminate the need for them entirely.
Q: How is the accuracy of the simulation model ensured?
A: Accuracy is ensured through three measures: ① Parameter calibration—model parameters are calibrated using measurement data from the test bench (e.g., component stiffness, damping, inertia); ② Closed-loop data feedback—data from every physical test is fed back into the simulation model to correct deviations between the model and actual performance; ③ Third-party validation—key model results are blind-tested by an independent testing team. After sufficient iteration, the deviation between simulated and measured key dynamic responses can be kept within 5%.
Q: How does the verification system align with GB standards and ISO standards?
A: Kelude's verification system is fully aligned with ISO 4301 Crane Design Standard, GB/T 25710-2010 Cranes — Test Specification and Procedures, and ISO 13849 Safety of Machinery — Safety-Related Parts of Control Systems. During the test case design phase, each standard clause is mapped to at least one simulation or physical test case. For ISO 13849, safety functions of the control system—such as emergency shutdown, torque limiting, and overspeed protection—are designed and validated against the required PLr grade. ISO 13849-1:2023 ISO 4301 GB/T 25710-2010

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