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LightForce Photon-Pressure Collision Avoidance: Updated Efficiency Analysis Utilizing a Highly Parallel Simulation ApproachThis paper provides an updated efficiency analysis of the LightForce space debris collision avoidance scheme. LightForce aims to prevent collisions on warning by utilizing photon pressure from ground based, commercial off the shelf lasers. Past research has shown that a few ground-based systems consisting of 10 kilowatt class lasers directed by 1.5 meter telescopes with adaptive optics could lower the expected number of collisions in Low Earth Orbit (LEO) by an order of magnitude. Our simulation approach utilizes the entire Two Line Element (TLE) catalogue in LEO for a given day as initial input. Least-squares fitting of a TLE time series is used for an improved orbit estimate. We then calculate the probability of collision for all LEO objects in the catalogue for a time step of the simulation. The conjunctions that exceed a threshold probability of collision are then engaged by a simulated network of laser ground stations. After those engagements, the perturbed orbits are used to re-assess the probability of collision and evaluate the efficiency of the system. This paper describes new simulations with three updated aspects: 1) By utilizing a highly parallel simulation approach employing hundreds of processors, we have extended our analysis to a much broader dataset. The simulation time is extended to one year. 2) We analyze not only the efficiency of LightForce on conjunctions that naturally occur, but also take into account conjunctions caused by orbit perturbations due to LightForce engagements. 3) We use a new simulation approach that is regularly updating the LightForce engagement strategy, as it would be during actual operations. In this paper we present our simulation approach to parallelize the efficiency analysis, its computational performance and the resulting expected efficiency of the LightForce collision avoidance system. Results indicate that utilizing a network of four LightForce stations with 20 kilowatt lasers, 85% of all conjunctions with a probability of collision Pc > 10 (sup -6) can be mitigated.
Document ID
20150000244
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Stupl, Jan
(SGT, Inc. Moffett Field, CA, United States)
Faber, Nicolas
(SGT, Inc. Moffett Field, CA, United States)
Foster, Cyrus
(SGT, Inc. Moffett Field, CA, United States)
Yang, Fan Yang
(Science and Technology Corp. Moffett Field, CA, United States)
Nelson, Bron
(Computer Sciences Corp. Moffett Field, CA, United States)
Aziz, Jonathan
(Colorado Univ. Boulder, CO, United States)
Nuttall, Andrew
(Stanford Univ. Stanford, CA, United States)
Henze, Chris
(NASA Ames Research Center Moffett Field, CA United States)
Levit, Creon
(NASA Ames Research Center Moffett Field, CA United States)
Date Acquired
January 8, 2015
Publication Date
September 9, 2014
Subject Category
Space Transportation And Safety
Report/Patent Number
ARC-E-DAA-TN17747
Report Number: ARC-E-DAA-TN17747
Meeting Information
Meeting: AMOS: Advanced Maui Optical and Space Surveillance Conference
Location: Wailea, Hawaii
Country: United States
Start Date: September 9, 2014
End Date: September 12, 2014
Sponsors: Maui Economic Development Board, Inc.
Funding Number(s)
CONTRACT_GRANT: NNX13AJ38A
CONTRACT_GRANT: NNX14AF94A
CONTRACT_GRANT: NNA10DF26C
CONTRACT_GRANT: NNA13AC87C
CONTRACT_GRANT: NNA08CG83C
CONTRACT_GRANT: NNA07CA29C
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
space debris mitigation
conjunction analysis
laser
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