Experimental validation of damping properties and solar pressure effects on flexible, high area-to-mass ratio debris model

Multilayer insulation (MLI) is a recently-discovered type of debris originating from delamination of aging spacecraft; it is mostly detected near the geosynchronous orbit (GEO). Observation data indicates that these objects are characterised by high reflectivity, high area-to-mass ratio (HAMR), fast rotation, high sensitivity to perturbations (especially solar radiation pressure) and change of area-to-mass ratio (AMR) over time. As a result, traditional models (e.g. cannonball) are unsuitable to represent and predict this debris' orbital evolution. Previous work by the authors effectively modelled the flexible debris by means of multibody dynamics to improve the prediction accuracy. The orbit evolution with the flexible model resulted significantly different from using the rigid model. This paper aims to present a methodology to determine the dynamic properties of thin membranes with the purpose to validate the deformation characteristics of the flexible model. A high-vacuum chamber (10−4 mbar) to significantly decrease air friction, inside which a thin membrane is hinged at one end but free at the other provides the experimental setup. A free motion test is used to determine the damping characteristics and natural frequency of the thin membrane via logarithmic decrement and frequency response. The membrane can swing freely in the chamber and the motion is tracked by a static, optical camera, and a Kalman filter technique is implemented in the tracking algorithm to reduce noise and increase the tracking accuracy of the oscillating motion. Then, the effect of solar radiation pressure on the thin membrane is investigated: a high power spotlight (500–2000 W) is used to illuminate the sample and any displacement of the membrane is measured by means of a high-resolution laser sensor. Analytic methods from the natural frequency response and Finite Element Analysis (FEA) including multibody simulations of both experimental setups are used for the validation of the flexible model by comparing the experimental results of amplitude decay, natural frequencies and deformation. The experimental results show good agreement with both analytical results and finite element methods.

[1]  Tim Flohrer,et al.  Properties of the high area-to-mass ratio space debris population at high altitudes , 2006 .

[2]  Thomas Schildknecht,et al.  Attitude Motion of Space Debris Objects under Influence of Solar Radiation Pressure and Gravity , 2012 .

[3]  G. Batchelor,et al.  An Introduction to Fluid Dynamics , 1968 .

[4]  Jacqueline A. Townsend,et al.  Mechanical Properties Degradation of Teflon ® FEP Returned From the Hubble Space Telescope , 1998 .

[5]  J. Liou,et al.  Orbital Dynamics of High Area-To-Mass Ratio Debris and Their Distribution in the Geosynchronous Region , 2005 .

[6]  Florin Moldoveanu,et al.  Kalman Filter Based Tracking in an Video Surveillance System , 2010 .

[7]  William H. Melbourne,et al.  Wind loading of structures , 1998 .

[8]  T. R. Bedding,et al.  Dynamics of a double pendulum with distributed mass , 2008, 0812.0393.

[9]  Moriba K. Jah,et al.  Coupled orbit–attitude motion of high area-to-mass ratio (HAMR) objects including efficient self-shadowing , 2014 .

[10]  Florent Deleflie,et al.  Semi-analytical theory of mean orbital motion for geosynchronous space debris under gravitational influence , 2009 .

[11]  T. Başar,et al.  A New Approach to Linear Filtering and Prediction Problems , 2001 .

[12]  C. Jung,et al.  The Red Book , 2009 .

[13]  T. Schildknecht,et al.  Color Photometry and Light Curve Observations of Space Debris , 2008 .

[14]  Mohinder S. Grewal,et al.  Kalman Filtering: Theory and Practice Using MATLAB , 2001 .

[15]  Luciano Anselmo,et al.  Analytical and semi-analytical investigations of geosynchronous space debris with high area-to-mass ratios , 2008 .

[16]  D. Vallado Fundamentals of Astrodynamics and Applications , 1997 .

[17]  Toshiya Hanada,et al.  Micro-satellite impact tests to investigate multi-layer insulation fragments , 2009 .

[18]  Thomas Schildknecht,et al.  Variation of Area-to-Mass-Ratio of HAMR Space Debris Objects , 2011 .

[19]  Gianmarco Radice,et al.  A Deformation Model of Flexible, High Area-To-Mass Ratio Debris for Accurate Propagation under Perturbation , 2014 .

[20]  Anne Lemaitre,et al.  Semi-analytical investigations of high area-to-mass ratio geosynchronous space debris including Earth’s shadowing effects , 2008 .