Component Mode Synthesis (CMS)

Category: Structural Analysis | Integrated 2026-04-06
CAE visualization for substructuring cms theory - technical simulation diagram
Component Mode Synthesis (CMS)

Component Mode Synthesis (CMS): Theoretical Foundations

What is the CMS Method?

πŸ§‘πŸŽ“

Professor, what is the CMS method?


πŸŽ“

CMS (Component Mode Synthesis) is a technique that divides a large-scale structure into substructures (components), reduces the dynamic characteristics of each component using modal coordinates, and then assembles the whole.


πŸ§‘πŸŽ“

"Divide, reduce, and assemble"?


πŸŽ“

For example, directly solving a full-vehicle model (millions of DOF) requires enormous computation. With the CMS method:

1. Divide into substructures like body, engine, suspension, etc.

2. Reduce each substructure using eigenmodes + constraint modes (to hundreds of DOF)

3. Combine the reduced substructures and solve the whole system


πŸ§‘πŸŽ“

Millions of DOF are reduced to thousands!


πŸŽ“

Computation time can become less than 1/100. Particularly effective when many substructures are used repeatedly (e.g., different vehicle body variations).


Craig-Bampton Method

πŸŽ“

The most widely used CMS method is the Craig-Bampton method (1968). Each substructure is represented by two types of modes:


  • Fixed-Interface Eigenmodes β€” Internal eigenmodes with the interface fixed
  • Constraint Modes β€” Static deformation when each interface DOF is given a unit displacement

.


πŸ§‘πŸŽ“

So eigenmodes represent internal vibration, and constraint modes represent interface deformation.


πŸŽ“

Displacement of each substructure:

$$ \{u\} = [\Phi_f | \Psi_c] \begin{Bmatrix} \{q\} \\ \{u_b\} \end{Bmatrix} $$

$\{q\}$ are modal coordinates (tens to hundreds), $\{u_b\}$ are interface DOFs. Total DOFs are reduced to $\sum (n_{modes} + n_{boundary})$.


Advantages of the CMS Method

πŸŽ“
AdvantageExplanation
Significant reduction in computation timeReduces total DOFs to 1/10 to 1/1000
ParallelizationEach substructure can be computed independently
Efficient design changesChanging one substructure does not require recalculating others
Intellectual property protectionSuppliers can provide only reduced models without disclosing internal structure
πŸ§‘πŸŽ“

Interesting that it can be used for IP protection.


πŸŽ“

In the automotive supply chain, suspension manufacturers provide CMS reduced models to OEMs. OEMs can perform full-vehicle vibration analysis without seeing the internal structure.


Summary

πŸ§‘πŸŽ“

Let me organize the CMS method.


πŸŽ“

Key points:


  • Divide large-scale structures into substructures and reduce β€” DOFs to 1/10 to 1/1000
  • Craig-Bampton method is standard β€” Eigenmodes + Constraint modes
  • Significant reduction in computation time β€” Essential for full-vehicle NVH analysis
  • Flexible for design changes β€” Changes possible per substructure
  • IP protection β€” Share reduced models without disclosing internal structure

Coffee Break Yomoyama Talk

Hurty and Craig's Invention of "Solving by Parts"

The CMS (Component Mode Synthesis) method was developed by Hurty (1960) and Craig & Bampton (1968). It's a technique that divides large-scale models into substructures, reduces them using the eigenmodes of each part, and then couples them. The Craig-Bampton method combines fixed-interface modes (internal DOF reduction) and constraint modes (boundary DOF retention) and remains the most widely used CMS formulation today.

Computational Methods for Component Mode Synthesis (CMS)

Implementation of the Craig-Bampton Method

πŸ§‘πŸŽ“

Please explain the implementation steps of the Craig-Bampton method.


Step 1: Substructure Definition

  • Divide the structure into logical components
  • Define interface DOFs (connection points between components)

Step 2: Reduction of Each Component

  • Eigenfrequency analysis with fixed interface β†’ Fixed-interface eigenmodes $[\Phi_f]$
  • Static analysis giving unit displacement to each interface DOF β†’ Constraint modes $[\Psi_c]$
  • Calculate reduced mass/stiffness matrices

Step 3: Assembly of the Whole

  • Combine reduced matrices of each component via interface DOFs
  • Solve the overall eigenvalue problem

Nastran

```

SOL 103

CEND

SUBCASE 1

METHOD = 10

BEGIN BULK

$ Superelement definition

SELOC, 100, ... $ Substructure definition

SECONM, 100, ... $ Reduction

```

Nastran's superelement functionality is the industry standard for CMS.

Abaqus

```

*SUBSTRUCTURE GENERATE

*RETAINED NODAL DOFS

interface_nodes, 1, 6

*FREQUENCY

50, ,

*END STEP

```

Ansys

Substructuring analysis type in Workbench allows CMS reduction setup via GUI.

πŸ§‘πŸŽ“

Is Nastran's superelement the industry standard?


πŸŽ“

For automotive and aerospace CMS analysis, Nastran's superelement has overwhelming track record. There is an industry-standard format (OP2/OP4 files) for exchanging reduced matrices.


How to Determine the Number of Modes to Retain

πŸ§‘πŸŽ“

How many fixed-interface eigenmodes should be retained?


πŸŽ“

Retain modes up to 1.5 to 2 times the frequency of the range of interest. For example, for full-vehicle analysis up to 500 Hz, retain modes up to 750~1000 Hz for each substructure.


Summary

πŸ§‘πŸŽ“

Let me organize the numerical methods of CMS.


πŸŽ“

Key points:


  • Craig-Bampton method β€” Reduction using fixed-interface eigenmodes + constraint modes
  • Nastran superelement is industry standard β€” OP2/OP4 format
  • Number of modes = up to 1.5~2 times the frequency of interest β€” Balance accuracy and computational cost
  • Interface DOF definition is key β€” Appropriate interface selection affects accuracy

Coffee Break Yomoyama Talk

Craig-Bampton Reduction Procedure and Accuracy Verification

The Craig-Bampton method involves three steps: β‘  Eigenmode calculation for internal DOFs (typically 0~f_max range) β‘‘ Constraint mode calculation by applying unit displacement to boundary DOFs β‘’ Assembly of reduced matrices. The standard procedure is to incorporate the reduced model into the full system, calculate eigenvalues, and verify accuracy within Β±1% compared to the full FEM. The cutoff frequency for internal eigenmodes uses 1.5 to 2 times the evaluation upper limit.

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