Aerocapture Guidance Algorithm Development and Testing
@inproceedings{Masciarelli2007AerocaptureGA, title={Aerocapture Guidance Algorithm Development and Testing}, author={James P. Masciarelli}, year={2007} }
An analytic predictor corrector guidance algorithm has been developed and tested for aerocapture at se veral destinations in our solar system, and proposed for demon stration through an Earth based flight test. This paper gives an overview of the guidance algorithm and results of simulation tests at Earth, Mars, Titan, Neptune, and Venus.
6 Citations
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A three-phase hybrid guidance law combined with constant bank angle profile algorithm, feedback linearization tracking algorithm and numerical predictor-corrector algorithm is proposed and demonstrates that the proposed method reaches the target orbit accurately and relieves the overload efficiently.
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Aerocapture is an orbit insertion maneuver in which a spacecraft flies through a planetary atmosphere one time using drag force to decelerate and effect a hyperbolic to elliptical orbit change.…
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In this work, a direct force control numerical pred ictor-corrector guidance architecture is developed to enable Neptune aerocapture using flight-heritage blunt body aeroshells. A linear aerodynamics…
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Atmospheric skip-entry trajectories are designed for the Lunar-return missions for new vehicles with low-lift-to-drag L/D ratios. Moreover, modern requirements, such as the diverse option of…
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