Force limiting: Test your Spacecraft, but don’t destroy it!

Due to its high value, satellite vibration qualification tests are among the most monitored and carefully conducted tests in the world. Since these tests are performed on real flight hardware, avoiding over-testing is of critical importance as it can result in unnecessary destruction of unwanted fatigue of the test specimen. Unfortunately, the industry is full of examples where satellites and spacecraft have been damaged during such tests.

To protect these one-of-a-kind or expensive test objects notching or limiting is used to prevent over-testing and excessive loading of the satellite or spacecraft structure. This is done by limiting the response levels at key locations on the test item or on the shaker system by reducing the drive signal at the offending frequencies.

However, notching also carries the risk of under-testing the spacecraft with all possible consequences during launch or use in space. Especially notching that is performed to limit local accelerations for the purpose of protecting equipment, instruments or subsystems is therefore always agreed with the customer when it can be proven that unreasonable over-testing will occur if not applied.

On the other hand, “force limiting”, as notching is called when applied to force, is the most widely accepted method of notching within the aerospace industry. It is a relatively new technology, first put in use at the Jet Propulsion Laboratory in 1990 after the mechanical failure of an aerospace component during a vibration test. Today force limiting is used in almost every major space lab worldwide. The basic ideas behind force limitation have been in the literature for decades, but the emergence of piezoelectric force transducers needed to easily implement force limitation has accelerated the implementation of the method over the last decades.

One of the most advanced Force Measurement Device (FMD) is in use at the European Space Agency and uses in total up to 24 individual tri-axial 24 force-links measured on a state-of-the-art start Siemens controller system.


Bepi Colombo spacecraft tested on QUAD shaker W640

ESA source: Bepi-Colombo spacecraft tested on Quad shaker with
FMD for force and moment limiting providing additional protection


FMD setup configuration for Force and Moment Limiting

A typical FMD consists of two rings connected by force links that each measure the dynamic forces in the three directions. The signals are conditioned by charge amplifiers and the outputs are then combined in real-time by a computing unit generating three forces and three moments. These six output channels are then available for either data acquisition or for vibration level control. These configurations are very reliable and have demonstrated safe spacecraft qualification testing.

More robust FMD setup configuration for safer spacecraft testing

New advances in vibration test system technology provide further protection for high-value test articles. Up-to-date Simcenter Testlab software supports a more robust FMD setup configuration for force and moment limiting by getting rid of the need for external conditioning units and summation hardware.

FMD4 1

Upper image: Configuration with FMD output connected to external charge conditioning units and force summation box.
Lower image: Configuration with FMD output signals directly connected to VCF4 modules of Simcenter SCADAS
controller with embedded global force and moment calculation in Simcenter Testlab software.


By extending the data acquisition capability of the Simcenter SCADAS hardware with the Simcenter SCADAS VCF4 module, force cells from the FMD can be connected directly to the control system omitting the need for external charge conditioning boxes. This arrangement immediately detects faulty load cells and thereby eliminates the risk of notching on inaccurate resulting force and moment signals.

The global forces and moments are generated within Siemens Testlab software using derived software channels, eliminating the need for summation boxes or real-time platforms. Moreover, the derivation of the equations for the forces and moments is simplified thanks to a geometry-based tool that allows deriving this automatically, which means a lot of relief for the user

This integrated solution, with minimal external hardware, clearly provides a much simpler. cheaper and more robust solution for satellite qualification testing


Simcenter SCADAS systems at Airbus Defense and Space are equipped with Simcenter SCADAS VCF4 modules for direct connection of FMD force channels or other types of sensors


 Source: Simcenter Blog, written by Mostapha_C




To learn more about Simcenter and to keep up with the latest from Dipolo, subscribe to our newsletter.