3D Profile Reconstruction and Guidance for the Terminal Area Energy Management Phase of an Unpowered RLV with Aerosurface Failure
Publication: Journal of Aerospace Engineering
Volume 33, Issue 3
Abstract
This paper focuses on the guidance of an unpowered reusable launch vehicle (RLV) with aerosurface failure in the terminal area energy management (TAEM) phase. The aerosurface failure will limit the bank capability, and has a great influence on the range and turning radius of RLV. To this end, a new TAEM guidance scheme with the ability of online profile reconstruction is proposed in this paper for the bank-constrained RLV. The 3-dimensional (3D) profile is reconstructed online by directly adjusting the parameters of the dynamic pressure profile and the two-external-tangent-circle-based ground track profile. As the coupling between vertical and lateral motion is considered in the trajectory propagation, the reconstruction accuracy is guaranteed. Then, a closed-loop TAEM guidance law is proposed to track the reconstructed 3D profile. The effectiveness and robustness of the guidance scheme are verified by numerical simulations with a variety of initial states and model deviations.
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Acknowledgments
This work was supported by National Natural Science Foundation of China (Grant No. 61803111).
References
Burchett, B. T. 2004. “Fuzzy logic trajectory design and guidance for terminal area energy management.” J. Spacecraft Rockets 41 (3): 444–450. https://doi.org/10.2514/1.10938.
Darwin, C. R., G. Austin, L. Varnado, and G. Eudy. 1991. “A view toward future launch vehicles: A civil perspective.” Acta Astronaut. 25 (3): 165–175. https://doi.org/10.1016/0094-5765(91)90144-T.
Freeman, D. C., T. A. Talay, and R. E. Austin. 1997. “Reusable launch vehicle technology program.” Acta Astronaut. 41 (11): 777–790. https://doi.org/10.1016/S0094-5765(97)00197-5.
Grantham, K. 2003. “Adaptive critic neural network based terminal area energy management/entry guidance.” In Proc., Aerospace Sciences Meeting and Exhibit. Reston, VA: American Institute of Aeronautics and Astronautics.
Hall, C. E., and Y. B. Shtessel. 2006. “Sliding mode disturbance observer-based control for a reusable launch vehicle.” J. Guidance Control Dyn. 29 (6): 1315–1328. https://doi.org/10.2514/1.20151.
Hanson, J. M., and R. E. Jones. 2004. “Test results for entry guidance methods for space vehicles.” J. Guidance Control Dyn. 27 (6): 960–966. https://doi.org/10.2514/1.10886.
Harl, N., and S. N. Balakrishnan. 2010. “Reentry terminal guidance through sliding mode control.” J. Guidance Control Dyn. 33 (1): 186–199. https://doi.org/10.2514/1.42654.
Hull, J., N. Gandhi, and J. Schierman. 2005. “In-flight TAEM/final approach trajectory generation for reusable launch vehicles.” In Proc., Infotech at Aerospace. Reston, VA: American Institute of Aeronautics and Astronautics.
Jiang, W., and Z. Yang. 2014. “Guidance law design for terminal area energy management of reusable launch vehicle by energy-to-range ratio.” Math. Prob. Eng. 2014 (4): 5–12. https://doi.org/10.1155/2014/929731.
Kluever, C., and K. Horneman. 2005. “Terminal trajectory planning and optimization for an unpowered reusable launch vehicle.” In Proc., AIAA Guidance, Navigation, and Control Conf. and Exhibit. Reston, VA: American Institute of Aeronautics and Astronautics.
Kluever, C., K. Horneman, and J. Schierman. 2009. “Rapid terminal-trajectory planner for an unpowered reusable launch vehicle.” In Proc., AIAA Guidance, Navigation, and Control Conf. Reston, VA: American Institute of Aeronautics and Astronautics.
Kluever, C. A. 2004. “Unpowered approach and landing guidance using trajectory planning.” J. Guidance Control Dyn. 27 (6): 967–974. https://doi.org/10.2514/1.7877.
Kluever, C. A. 2007. “Terminal guidance for an unpowered reusable launch vehicle with bank constraints.” J. Guidance Control Dyn. 30 (1): 162–168. https://doi.org/10.2514/1.24864.
Kluever, C. A., and D. A. Neal. 2015. “Approach and landing range guidance for an unpowered reusable launch vehicle.” J. Guidance Control Dyn. 38 (11): 2057–2066. https://doi.org/10.2514/1.G000909.
Lan, X. J., L. Liu, and Y. J. Wang. 2016. “Online trajectory planning and guidance for reusable launch vehicles in the terminal area.” Acta Astronaut. 118 (Jan–Feb): 237–245. https://doi.org/10.1016/j.actaastro.2015.10.019.
Li, M., and J. Hu. 2018. “An approach and landing guidance design for reusable launch vehicle based on adaptive predictor–corrector technique.” Aerosp. Sci. Technol. 75 (Apr): 13–23. https://doi.org/10.1016/j.ast.2017.12.037.
Liang, Z., Q. Li, and Z. Ren. 2016. “Onboard planning of constrained longitudinal trajectory for reusable launch vehicles in terminal area.” Adv. Space Res. 57 (3): 742–753. https://doi.org/10.1016/j.asr.2015.11.027.
Mayanna, A., W. Grimm, and K. Well. 2006. “Adaptive guidance for terminal area energy management (TAEM) of reentry vehicles.” In Proc., AIAA Guidance, Navigation, and Control Conf. and Exhibit. Reston, VA: American Institute of Aeronautics and Astronautics.
Morio, V., F. Cazaurang, A. Falcoz, and P. Vernis. 2010. “Robust terminal area energy management guidance using flatness approach.” IET Control Theory Appl. 4 (3): 472–486. https://doi.org/10.1049/iet-cta.2008.0463.
Mu, L., X. Yu, Y. M. Zhang, P. Li, and X. Wang. 2018. “Onboard guidance system design for reusable launch vehicles in the terminal area energy management phase.” Acta Astronaut. 143 (Feb): 62–75. https://doi.org/10.1016/j.actaastro.2017.10.027.
Ridder, S. D., and E. Mooij. 2011a. “Optimal longitudinal trajectories for reusable space vehicles in the terminal area.” J. Spacecraft Rockets 48 (4): 642–653. https://doi.org/10.2514/1.51083.
Ridder, S. D., and E. Mooij. 2011b. “Terminal area trajectory planning using the energy-tube concept for reusable launch vehicles.” Acta Astronaut. 68 (7): 915–930. https://doi.org/10.1016/j.actaastro.2010.08.032.
Tomatis, C., L. Bouaziz, T. Franck, and J. Kauffmann. 2009. “RLV candidates for European future launchers preparatory programme.” Acta Astronaut. 65 (1–2): 40–46. https://doi.org/10.1016/j.actaastro.2009.01.057.
Wei, X., X. Lan, L. Liu, and Y. Wang. 2019. “Rapid trajectory planning of a reusable launch vehicle for airdrop with geographic constraints.” Int. J. Adv. Rob. Syst. 16 (1): 1–14. https://doi.org/10.1177/1729881418817971.
You, M., Q. Zong, B. Tian, X. Zhao, and F. Zeng. 2018. “Comprehensive design of uniform robust exact disturbance observer and fixed-time controller for reusable launch vehicles.” IET Control Theory Appl. 12 (5): 638–648. https://doi.org/10.1049/iet-cta.2017.0466.
Zhou, M., J. Zhou, and J. G. Guo. 2015. “On-line trajectory planning and guidance for terminal area energy management of reusable launch vehicle.” J. Astronautics 36 (2): 151–157. https://doi.org/10.3873/j.issn.1000-1328.2015.02.004.
Zhou, M., J. Zhou, and Z. Guo. 2018. “Finite-time sliding mode based terminal area guidance with multiple constraints.” In Proc., 3rd Int. Conf. on Control and Robotics Engineering, 60–64. New York: IEEE.
Zhou, M., J. Zhou, and M. Lu. 2017. “Rapid longitudinal trajectory planning for RLVs in the terminal area.” In Proc., 29th Chinese Control and Decision Conf., 1634–1639. New York: IEEE.
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©2020 American Society of Civil Engineers.
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Received: Sep 12, 2018
Accepted: Sep 16, 2019
Published online: Feb 8, 2020
Published in print: May 1, 2020
Discussion open until: Jul 8, 2020
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