Refining space object radiation pressure modeling with bidirectional reflectance distribution functions

Charles J. Wetterer, Richard Linares, John Crassidis, Tom Kelecy, Marek Ziebart, Moriba Jah, Paul Cefola

Research output: Contribution to journalConference articlepeer-review

4 Scopus citations

Abstract

High fidelity orbit propagation requires detailed knowledge of the solar radiation pressure (SRP) on a space object. The SRP depends not only on the space object's shape and attitude, but also on the absorption and reflectance properties of each surface on the object. These properties are typically modeled in a simplistic fashion, but are here described by a surface bidirectional reflectance distribution function (BRDF). Several analytic BRDF models exist, and are typically complicated functions of illumination angle and material properties represented by parameters within the model. In general, the resulting calculation of the SRP would require a time consuming numerical integration. This might be impractical if multiple SRP calculations are required for a variety of material properties in real time, for example, in a filter where the particular surface parameters are being estimated. This paper develops a method to make accurate and precise SRP calculations quickly for some commonly used analytic BRDFs. Additionally, other non-gravitational radiation pressures exist including Earth albedo/Earth infrared radiation pressure, and thermal radiation pressure from the space object itself and are influenced by the specific BRDF. A description of these various radiation pressures and a comparison of the magnitude of the resulting accelerations at various orbital heights and the degree to which they affect the space object's orbit are also presented. Significantly, this study suggests that for space debris whose interactions with electro- magnetic radiation are described accurately with a BRDF, then hitherto unknown torques would account for rotational characteristics affecting both tracking signatures and the ability to predict the orbital evolution of the objects.

Original languageEnglish (US)
Pages (from-to)2699-2717
Number of pages19
JournalAdvances in the Astronautical Sciences
Volume148
StatePublished - 2013
Event23rd AAS/AIAA Space Flight Mechanics Meeting, Spaceflight Mechanics 2013 - Kauai, HI, United States
Duration: Feb 10 2013Feb 14 2013

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