Relevant bibliographies by topics / Aeroassist Maneuver

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  1. Journal articles
  2. Dissertations / Theses
  3. Conference papers

Academic literature on the topic 'Aeroassist Maneuver'

Author: Grafiati
Published: 4 June 2021
Last updated: 1 February 2022

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Journal articles on the topic "Aeroassist Maneuver"

1

Trask, Aaron J., and Victoria L. Coverstone. "Optimal Low-Thrust Trajectories Combined with an Aeroassist Maneuver." Journal of Spacecraft and Rockets 41, no. 4 (2004): 629–34. http://dx.doi.org/10.2514/1.2582.

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FUJITA, Kazuhisa, Takashi KUBOTA, Naoko OGAWA, et al. "Assessment of Aeroassist Orbital Maneuver Technologies for Next Mars Exploration." TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN 8, ists27 (2010): Pk_23—Pk_29. http://dx.doi.org/10.2322/tastj.8.pk_23.

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Mazzaracchio, Antonio. "Coupled versus uncoupled optimal solutions for thermal and dynamic problems in spacecraft atmospheric flight." World Journal of Engineering 13, no. 1 (2016): 53–60. http://dx.doi.org/10.1108/wje-02-2016-006.

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Purpose This paper aims to address a significant issue related to the coupled and uncoupled treatment of the thermal and dynamic problems in the optimization of aeroassisted orbital maneuvers and the simultaneous optimal sizing of the associated heat shields. The literature generally focuses on decoupled treatments that reduce the computational load; in this manner, consequently, a decrease in the representativity of the solution manifests. The general operating mode first optimizes the trajectory and subsequently defines the optimal heat shield design based on that trajectory. Design/methodol
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Gomes dos Santos, Willer, Evandro Marconi Rocco, and Valdemir Carrara. "Trajectory Control During an Aeroassisted Maneuver Between Coplanar Circular Orbits." Journal of Aerospace Technology and Management 6, no. 2 (2014): 159–68. http://dx.doi.org/10.5028/jatm.v6i2.351.

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Abd El-Salam, F. A. "Optimization out-of-orbit plane changes using aeroassisted maneuvers." Applied Mathematics and Computation 170, no. 2 (2005): 1303–13. http://dx.doi.org/10.1016/j.amc.2005.01.022.

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Elisov, N. A., S. A. Ishkov, and A. A. Khramov. "Application of differential evolution algorithm in the problem of aeroassisted orbital plane change maneuver." VESTNIK of Samara University. Aerospace and Mechanical Engineering 18, no. 4 (2020): 41–51. http://dx.doi.org/10.18287/2541-7533-2019-18-4-41-51.

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The paper deals with application of the differential evolution method in optimizing aeroassisted orbital plane change maneuver performed by an aerospace vehicle with a high lift-to-drag ratio. The vehicle’s motion relative to the Earth is described by a system of differential equations in the flight path axis system. The angle-of-attack and the air path bank angle control programs are presented in the form of Fourier series and thrust control has the form of flip-flop control. The results of solving problems without phase parameter constraints obtained by the differential evolution algorithm w
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Speyer, Jason L., and Edwin Z. Crues. "Approximate optimal atmospheric guidance law for aeroassisted plane-change maneuvers." Journal of Guidance, Control, and Dynamics 13, no. 5 (1990): 792–802. http://dx.doi.org/10.2514/3.25404.

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ELISOV, Nikolay A., Sergey A. ISHKOV, Igor A. LOMAKA, and Valentin G. SHAKHOV. "Influence of non-equilibrium reactions on the optimization of aerothrust aeroassisted maneuver with orbital change." Chinese Journal of Aeronautics 33, no. 8 (2020): 2133–45. http://dx.doi.org/10.1016/j.cja.2020.04.016.

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Han, Hongwei, and Dong Qiao. "Optimization for the Aeroassisted Orbital Plane Change with the Synergetic Maneuver Using the hp-Adaptive Pseudospectral Method." Journal of Aerospace Engineering 30, no. 6 (2017): 04017076. http://dx.doi.org/10.1061/(asce)as.1943-5525.0000788.

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Mazzaracchio, Antonio. "Thermal Protection System and Trajectory Optimization for Orbital Plane Change Aeroassisted Maneuver." Journal of Aerospace Technology and Management 5, no. 1 (2013). http://dx.doi.org/10.5028/jatm.v5i1.208.

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Dissertations / Theses on the topic "Aeroassist Maneuver"

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(7116044), Ye Lu. "Planetary Mission Design and Analysis Using Aeroassist Maneuvers." Thesis, 2019.

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<div>Mission designs have been focused on using proven orbital maneuvers (i.e., propulsive maneuvers and gravity-assist) to deliver spacecraft to planetary destinations. Aeroassist maneuvers, despite their potential benefits, have not been given serious considerations due to the perceived risk and complexity. As entry technologies mature, aeroassist maneuvers need to be considered more extensively. Currently, there is no tool available that can perform rapid preliminary mission designs using aeroassist maneuvers. In this dissertation, integrated design methodologies for aerocapture and aerogra
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(10587056), Rohan Gajanan Deshmukh. "System Analysis of a Numerical Predictor-Corrector Aerocapture Guidance Architecture." Thesis, 2021.

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<p>Aerocapture has been envisioned as a potential orbit insertion technique for planetary destinations with an atmosphere. Despite not being flight proven technique, many studies found in the literature and recent mission proposals have employed aerocapture into their respective mission designs. The potential varying levels of trajectory dispersions experienced during atmospheric flight at each destination drives the need for robust and fuel-efficient guidance and control solutions. Existing guidance algorithms have relied on tracking precomputed reference trajectories, which are computed usin
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3

(11068791), Athul Pradeepkumar Girija. "A Systems Framework and Analysis Tool for Rapid Conceptual Design of Aerocapture Missions." Thesis, 2021.

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Aerocapture offers a near propellantless and quick method of orbit insertion at atmosphere bearing planetary destinations. Compared to conventional propulsive insertion, the primary advantage of using aerocapture is the savings in propellant mass which could be used to accommodate more useful payload. To protect the spacecraft from the aerodynamic heating during the maneuver, the spacecraft must be enclosed in a protective aeroshell or deployable drag device which also provides aerodynamic control authority to target the desired conditions at atmospheric exit. For inner planets such as
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Conference papers on the topic "Aeroassist Maneuver"

1

ZHAO, Y., and W. GARRARD. "Piecewise-constant guidance for aeroassisted maneuvers." In Astrodynamics Conference. American Institute of Aeronautics and Astronautics, 1992. http://dx.doi.org/10.2514/6.1992-4643.

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2

MISHNE, D., and J. SPEYER. "Optimal control of aeroassisted plane change maneuver using feedbackexpansions." In Astrodynamics Conference. American Institute of Aeronautics and Astronautics, 1986. http://dx.doi.org/10.2514/6.1986-2136.

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SPEYER, JASON, and EDWIN CRUES. "An approximate atmospheric guidance law for aeroassisted plane change maneuvers." In Guidance, Navigation and Control Conference. American Institute of Aeronautics and Astronautics, 1988. http://dx.doi.org/10.2514/6.1988-4174.

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CALISE, ANTHONY, and NAHUM MELAMED. "Matched asymptotic expansion of the Hamilton-Jacobi-Bellman equationfor aeroassisted plane-change maneuvers." In Guidance, Navigation and Control Conference. American Institute of Aeronautics and Astronautics, 1993. http://dx.doi.org/10.2514/6.1993-3752.

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MCFARLAND, MICHAEL, and ANTHONY CALISE. "A hybrid approach to near-optimal atmospheric guidance for aeroassisted orbit transfer maneuvers." In Guidance, Navigation and Control Conference. American Institute of Aeronautics and Astronautics, 1993. http://dx.doi.org/10.2514/6.1993-3858.

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6

Mishne, D., and J. Speyer. "A guidance law for the aeroassisted plane change maneuver in the presence of atmospheric uncertainties." In 1986 25th IEEE Conference on Decision and Control. IEEE, 1986. http://dx.doi.org/10.1109/cdc.1986.267419.

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