Research on High Accuracy Guidance Law for Reentry Vehicles

Zhi Gang Wang; Shen Yan

doi:10.4028/www.scientific.net/AMM.427-429.81

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 427-429Research on High Accuracy Guidance Law for Reentry...

Research on High Accuracy Guidance Law for Reentry Vehicles

Abstract:

The problem of low accuracy for classic guidance law is considered in this paper. Based on the mature theory used in missiles, this paper presents an integrated guidance law for reentry vehicles. At the initial stage of reentry flight, standard trajectory guidance law is employed, and then converts to 3dof proportional guidance law when this vehicle is close to the target. Simulation results are provided to demonstrate the accuracy of the proposed integrated guidance law.

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Periodical:

Applied Mechanics and Materials (Volumes 427-429)

Pages:

81-84

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.427-429.81

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Online since:

September 2013

Authors:

Zhi Gang Wang*, Shen Yan

Keywords:

Integrated Guidance, Reentry Guidance, Reentry Vehicle, Terminal Guidance

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* - Corresponding Author

References

[1] Harpold. J. C, Graves. C. A, Jr, in: Shuttle Entry Guidance. The Journal of the Astronautical Sciences, 1979, XXV(3): 239-268.

Google Scholar

[2] Joshi. Ashok, Sivan. K , Amma.S. Savithri, in: Predictor-Corrector Reentry Guidance Algorithm with Path Constraints for Atmospheric Entry Vehicles. Journal of Guidance, Control and Dynamics, 2007, 30(5): 1307-1318.

DOI: 10.2514/1.26306

Google Scholar

[3] Greg.A. Dukeman: Profile-following entry Guidance using Linear Quadratic Regulator Theory. AIAA Guidance, Navigation, and Control Conference and Exhibit. 5-8 August 2002, Mnoterey, California.

DOI: 10.2514/6.2002-4457

Google Scholar

[4] Sivan K , Amma S. Savithri, Joshi Ashok, et al. An adaptive reentry guidance[R]. Indian: Indian Institute of Technology Bornbay, (2004).

Google Scholar

[5] Ping. Lu. Adaptive Terminal Guidance for Hypervelocity Impact in Specified Direction[R]. Journal of Guidance, Control and Dynamics, 2006, 29(2).

DOI: 10.2514/1.14367

Google Scholar