Multibody Dynamics Simulation




Concurrent Dynamics delivers high fidelity Multibody Dynamics Simulation programs to assess dynamics and control performances of mechanisms and mobile vehicles. They expedite:

  • Concept Feasibility Evaluation

  • Control System Design and Testing

  • Hardware-in-the-Loop Simulation

  • System Failure Analysis, etc..

Satellite 'Ibuki': courtesy of JAXA

MBS packages and dynamics formulation notes follow.


1.  MBS Packages

We have ready-to-use simulation packages for a variety of vehicles and operations. Beside the packages below, more are on the robotics page and in the works. The model equations in these packages are derived from Euler-Lagrange formulation. They run on PC's that have Matlab/Simulink or C/C++ Compilers installed. Their main program, XSV01,

  • Generates minimal state multibody dynamics equations for each vehicle or mechanism being simulated 

  • Solves the dynamics equations efficiently (by order(N) method) so you can concentrate on the design and testing of control systems

  • Connects easily with user defined control systems

  • Permits easy model/control system parameter modifications to achieve simulation goals quickly

Get a free Project license for any of the packages below by contacting Click 's' below for a synopsis of each package. Click 'm' for details on creating the model file using the editor, buildx.exe, and on the mdl file or the control.dll file designed for that application and more. We welcome suggestions on vehicle simulations that you would like to have.


XSV01 Packages for Simulink.

SV1sim: Simulates a vehicle with 4 wheels and 8 jets under a nominal rwa ACS and a jet ACS. The control task is to maintain vehicle attitude at  LVLH given some initial attitude disturbance. s, m 

Arraysim: Simulates an expanded version of SV1sim vehicle. It retains the same ACS, but now has two arrays each with a yoke and 3 panels. The control tasks include a coordinated array deployment using the 'gear' and 'lock' constraints and the maintenance of LVLH attitude with the ACS. s, m 

Sep1sim: Simulates the ejection of a satellite from a spinning mothership. The control tasks include ejecting the satellite, deploying the arrays after separation, followed by nulling the satellite rate and capturing LVLH attiude with jet ACS. The remainder of the simulation is to maintain LVLH attitude using RWA ACS. Examples show the VMASS (variable mass) feature of the simulation engine in managing a vehicle mass property discontinuity at the instant of the separation. s, m 

Tethersim: Simulates the deployment of a payload with a tether. Tether length and pushoff force are adjustable. Examples show a different system response between a small pld/vehicle mass ratio and a large such ratio. Successful deployment depends on several parameters. s, m 

CMG4sim: Simulates a vehicle with 4 SGCMG's and 8 jets. It has a nominal CMG ACS and a momentum management system. Examples show the ACS operations with/without momentum mgmt. Users can design different CMG mounting configurations and test the corresponding CMG ACS. LVLH control is shown, sun-nadir ACS can be done also. s, m 


C-programmable XSV01 Packages

Examples in these packages run on PC's that have C/C++ compilers installed. Each package has the program XSV01.exe  to run simulations based on a user specified model file and a user supplied  control.dll file for a user conceived application. Our editor, buildx.exe and application library make the programming of that control.dll file easy by creating a near functional template to accomodate user's control system. The user's manual in each package shows how  the model file is built and how the associated control.dll is programmed and compiled for each example.





















2.  Multibody Dynamics Notes


Kinematics of mechanisms is about computing the motion of bodies in the system given its generalized coordinates and rates. The motion include the attitude of bodies, their position and velocity over time. The coordinates for simple systems comprise of the attitude of the reference body, its cm inertial motion, and all angles between single-axis-joint connected bodies in the system. The coordinates for more complex system would include coordinates for 3 dof relative rotational and relative translational motions between bodies.

Click here to see the kinematics of a generic multibody system(MBS). 

Generalized Mass Matrix

One encounters generalized mass matrix in the study of the system kinetic energy, momentum and force equations of an MBS. This matrix is a second order partial derivative of the system kinetic energy with respect to the generalized rates. Obtaining this partial derivative can be challenging even for a small scale mechanism.

Click here to see a derivation of the generalized mass matrix of a multibody system in a factored form. In the process, the notion of incidence matrix is introduced to simplify the derivation of the mass matrix.

Newton-Euler Equations

Many formalisms exist to establish the equations of motion (EOM) of a multibody system. These include the Euler-Lagrange equations, D'Alembert's work principle, Newton-Euler equations and others. Regardless of the formulation method used, the final EOM for the targeted mechanism for the same generalized coordinates are identical. One variation in the EOM is that they could be formulated to solve for the system accelerations or for the time derivative of system momenta. Still, solving either form of EOM and propagating the motion with the associated kinematics equations should yield the same dynamics response when the modeled MBS is subjected to the same forces and torque (internal and external). Moreover, the EOM must comply with momentum conservation when no external force or  torque is applied.

Click here  to see the derivation of the EOM of  tree-configured systems using the Newton-Euler equations. Solving the accelerations in O(n) manner is presented. 

Hamilton's Equations

The Hamiltonian is the total energy of the system and it permits a transformation of the Lagrangian equations into a system of 2n first order differential equations in generalized coordinates and generalized momenta, n being the number of dof's in the system. These equations produce identical results as those by acceleration based EOM.

Click here  to see details of the Hamilton's equations and the numerical processes involved in using them for MBS dynamics simulations. O(n) method of the rate solution required by Hamilton's equations is presented. 

Joint Motion

Joints connect bodies in a mechanism and define the relative motion between them. It is the coordinated movements at these joints that creates the trajectory of the robot arm grapple device, the cyclic up and down motion of a piston in a combustion engine, and the precise placement or pointing of a device on a hexapod platform. Most mechanisms are designed with 1 dof rotational joints. Yet, it is not uncommon to see universal joints, ball joints or prismatic joints in mechanisms.

A common treatment of joint motion in a mathematical model is to assign 6 dof's to each body in the system and then define joint constraints to be satisfied by solving a large system of DAE's. This approach effectively creates a dynamics model that has the right number of dof's fitting the simulated mechanism. It has advantages and obvious drawbacks. The presentation given here avoids the use of Lagrange multipliers as required by this approach. We choose to derive only as many EOM's as there are degrees of freedom in the system. The advantage of the latter approach is self explanatory.

Notably, use of Lagrange multipliers for constraints compliance is a very important subject in many applications. This topic will be addressed later. 

Click here to see a presentation on the adjustments to the kinematic equations given earlier to accomodate multiple types of joint motion in a mechanism.

System Angular Momentum

Multibody system angular momentum has two important properties for trouble-shooting vehicle dynamics simulations. P1: It  is a state of motion given the vehicle's generalized coordinates and rates. P2: It is constant in the inertial space when no external torque is exerted on the system. P1 means that this state computed by the simulation program must be identical to an independently computed one based on the kinematical variables output from the program and mass property of the vehicle. Error in this test reflects inconsistency in the kinematics or in the mass property used by the simulation program. P2 compliance insures that the underlying dynamics formulation of the simulation is done properly. 

Click here to see three ways to compute the multibody system angular momentum based on how the position of member body cm's are defined by the simulation. This angular momentum is easy to compute in a post-sim or exo-sim manner. P1 and P2 compliances underscore the validity of any multibody dynamics simulation.


Click here to see selected papers and books published on multibody dynamics formulations since 1965.


See robotics/mechanisms page


Interesting Websites:

  1. Multibody System Dynamics- Research Activities ( )
  2. Space flight news ( )
  3. Review of multibody dynamics software ( )
  4. Aerospace news (
  5. Robotics news (



Concurrent Dynamics International
Last modified: February 28, 2016