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Copernicus-LinCov (COPCOV) Software Integration in Support of Robust Trajectory OptimizationRobust trajectory optimization is the process of optimizing a trajectory while accounting for system uncertainty due to a variety of potential error sources. This work highlights the development and features of a novel tool known as CopCov to support robust trajectory optimization efforts. CopCov acts as an interface between Copernicus, a generalized trajectory design and optimization tool, and LinCov, a linear covariance analysis tool. By having a direct interface between these two software packages, Copernicus can receive covariance information from LinCov through a direct feedback loop, thus enabling optimization of a trajectory that is robust to trajectory dispersions and navigation errors. This paper details the architecture of CopCov and its flexibility to operate under varying configurations, including with both tools running locally or alternatively with the tools communicating via a remote connection. Additionally, the CopCov tool is demonstrated on a simple Hohmann transfer reference trajectory with varying numbers of Trajectory Correction Maneuvers (TCMs) and varying problem formulations. This example scenario is used to highlight how the inclusion of the CopCov interface affects burn placement of both major burns and minor burns (i.e., TCMs) in the optimized solution. Results are compared against analytical solutions and against a Genetic Algorithm (GA) optimizer for independent verification and validation.
Document ID
20230010563
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Joshua K. Geiser
(Johnson Space Center Houston, Texas, United States)
David Woffinden
(Johnson Space Center Houston, Texas, United States)
Matt Horstman
(Jacobs (United States) Dallas, Texas, United States)
Date Acquired
July 18, 2023
Subject Category
Astrodynamics
Report/Patent Number
AAS 23-128
Meeting Information
Meeting: AAS/AIAA Astrodynamics Specialist Conference
Location: Big Sky, MT
Country: US
Start Date: August 13, 2023
End Date: August 17, 2023
Sponsors: American Institute of Aeronautics and Astronautics, American Astronautical Society
Funding Number(s)
WBS: 804911.02.05.3491.23
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
Single Expert
Keywords
Copernicus
LinCov
trajectory design
robust trajectory optimization
trajectory optimization
linear covariance
orbital mechanics
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