Review and assessment of the steep lifting entry closed-form trajectory solution

Zachary R Putnam, Robert D. Braun

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

The complete, historical closed-form steep lifting entry trajectory solution is documented and developed from first principles. The efficacy and accuracy of the solution is assessed for application to aeroassist missions of interest, including aerocapture and en- try. Specifically, analytical assessment of the primary assumptions in the solution shows the solution is applicable across a wide range of initial states for vehicles with nonzero lift-to-drag ratios. Solution accuracy is assessed relative to the planar equations of motion; accuracy improves for steeper trajectories and larger lift-to-drag ratios. The steep lifting entry estimate of peak acceleration is shown to be accurate to within 10% for initial flight- path angles steeper than approximately -10 deg across a variety of vehicles, missions, and planetary destinations. Overall, the steep lifting entry solution provides a simple, rapid first-order trajectory solution capability for lifting aeroassist vehicles with relatively steep initial flight-path angles.

Original languageEnglish (US)
Title of host publicationAIAA Atmospheric Flight Mechanics Conference
PublisherAmerican Institute of Aeronautics and Astronautics Inc, AIAA
ISBN (Print)9781624103902
StatePublished - Jan 1 2016
EventAIAA Atmospheric Flight Mechanics Conference, 2016 - San Diego, United States
Duration: Jan 4 2016Jan 8 2016

Publication series

NameAIAA Atmospheric Flight Mechanics Conference

Other

OtherAIAA Atmospheric Flight Mechanics Conference, 2016
CountryUnited States
CitySan Diego
Period1/4/161/8/16

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ASJC Scopus subject areas

  • Aerospace Engineering
  • Energy Engineering and Power Technology
  • Mechanical Engineering
  • Computer Science Applications

Cite this

Putnam, Z. R., & Braun, R. D. (2016). Review and assessment of the steep lifting entry closed-form trajectory solution. In AIAA Atmospheric Flight Mechanics Conference (AIAA Atmospheric Flight Mechanics Conference). American Institute of Aeronautics and Astronautics Inc, AIAA.