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Partial Derivatives of the Lambert ProblemA procedure for deriving analytic partial derivatives of the Lambert problem is presented. Using the universal, cosine based Lambert formulation; first order partial derivatives of the velocities with respect to the positions and times are developed. Taking advantage of inherent symmetries and intermediate variables, the derivatives are expressed in a computationally efficient form. The added cost of computing these partials is found to be approximately 10% to approximately 60% of the Lambert compute cost. The availability of analytic partial derivatives increases optimization speed, efficiency and allows for trajectory optimization formulations that implicitly enforce continuity constraints via embedded Lambert problems.





Document ID
20160008235
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
External Source(s)
Authors
Arora, Nitin
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Russell, Ryan P.
(Texas Univ. Austin, TX, United States)
Strange, Nathan
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
July 1, 2016
Publication Date
August 5, 2014
Subject Category
Astrodynamics
Meeting Information
Meeting: AIAA SPACE 2014 Conference and Exposition
Location: San Diego, CA
Country: United States
Start Date: August 5, 2014
End Date: August 7, 2014
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Other
Keywords
trajectory computation

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