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SCIENCE CHINA Information Sciences, Volume 62, Issue 1: 010206(2019) https://doi.org/10.1007/s11432-018-9547-4

Trajectory optimization for RLV in TAEM phase using adaptive Gauss pseudospectral method

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  • ReceivedJun 23, 2018
  • AcceptedJul 10, 2018
  • PublishedDec 14, 2018

Abstract

There is no abstract available for this article.


Acknowledgment

This work was supported by China Postdoctoral Science Foundation (Grant No. 2017M620858). The authors would like to greatly appreciate the editor and all the anonymous reviewers for their comments, which helped to improve the quality of this letter.


References

[1] Horneman K, Kluever C. Terminal area energy management trajectory planning for an unpowered reusable launch vehicle. In: Proceedings of AIAA Atmospheric Flight Mechanics Conference and Exhibit, 2004. 5183. Google Scholar

[2] Kluever C, Horneman K. Terminal trajectory planning and optimization for an unpowered reusable launch vehicle. In: Proceedings of AIAA Guidance, Navigation, and Control Conference and Exhibit, 2005. 6058. Google Scholar

[3] De Ridder S, Mooij E. Terminal area trajectory planning using the energy-tube concept for reusable launch vehicles. Acta Astronaut, 2011, 68: 915-930 CrossRef ADS Google Scholar

[4] Mu L, Yu X, Zhang Y M. Onboard guidance system design for reusable launch vehicles in the terminal area energy management phase. Acta Astronaut, 2018, 143: 62-75 CrossRef ADS Google Scholar

[5] Guo L, Gao B, Li Y. A fast algorithm for nonlinear model predictive control applied to HEV energy management systems. Sci China Inf Sci, 2017, 60: 092201 CrossRef Google Scholar

[6] Tian B, Fan W, Su R. Real-Time Trajectory and Attitude Coordination Control for Reusable Launch Vehicle in Reentry Phase. IEEE Trans Ind Electron, 2015, 62: 1639-1650 CrossRef Google Scholar

  • Figure 1

    (Color online) Simulation diagrams of TAEM trajectory based on AGPM. (a) Altitude; (b) longitude; (c) latitude; (d) velocity; (e) flight path angle; (f) heading angle; (g) the 3D-surface plots of the drag coefficient; (h) the 3D-surface plots of the lift coefficient; and (i) the 3D path of the generated TAEM trajectory.

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