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2021 | OriginalPaper | Chapter

13. Omnidirectional Autonomous Reentry Guidance Based on 3-D Analytical Glide Formulae Considering Influence of Earth’s Rotation

Authors : Wanchun Chen, Hao Zhou, Wenbin Yu, Liang Yang

Published in: Steady Glide Dynamics and Guidance of Hypersonic Vehicle

Publisher: Springer Singapore

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Abstract

Common Aero Vehicle (CAV) is a high-L/D hypersonic vehicle gliding in the region of the Earth’s atmosphere with altitude of 20–100 km. CAV is sent into a sub-orbital trajectory by a launch vehicle. After separating from the launch vehicle, CAV reenters the atmosphere with initial Mach number of about 20. As the maximum L/D (L/Dmax) is up to 3, CAV can travel more than ten thousand kilometers, while its lateral maneuver range can also be up to thousands of kilometers. The flight of CAV can be roughly divided into entry and nosedive phases. In the entry phase, CAV manages the flight energy by performing proper lateral maneuvers, and eliminates the heading error by conducting several bank reversals.

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previous chapter 3-D Reentry Guidance with Real-Time Planning of Reference using New Analytical Solutions Based on Spectral Decomposition Method
next chapter Analytical Steady-Gliding Guidance Employing Pseudo-Aerodynamic Profiles
Appendix
Available only for authorised users
Literature
1.
Phillips T.H. A common aero vehicle (CAV) model, description, and employment guide. Schafer Corporation for AFRL and AFSPC. (2003)
2.
Xiong, S., Wang, W., Liu, X., et al.: Guidance law against maneuvering targets with intercept angle constraint. ISA Trans. 53(4), 1332–1342 (2014)CrossRef
3.
Yu, W., Chen, W.: Trajectory-shaping guidance with final speed and load factor constraints. ISA Trans. 56, 42–52 (2015a)CrossRef
4.
Wang, X., Zhang, Y., Wu, H.: Sliding mode control based impact angle control guidance considering the seeker’s field-of-view constraint. ISA Trans. 61, 49–59 (2016)CrossRef
5.
Harpold, J.C., Graves, C.A.: Shuttle Entry Guidance. NASA Lyndon B. Johnson Space Center, Houston (1979)
6.
Eggers, A.J., Allen, H.J., Neice, S.E. A Comparative Analysis of the Performance of Long-range Hypervelocity Vehicles. National Advisory Committee for Aeronautics. (1957)
7.
Gazley, C. Atmospheric entry. The RAND Corporation (1960)
8.
Lees, L., Hastwig, F.W., Cohen, C.B.: Use of aerodynamic lift during entry into the earth’s atmosphere. ARS J. 29(9), 633–641 (1959)CrossRef
9.
Ting, L., Wang, K.: An approximate analytic solution of re-entry trajectory with aerodynamic forces. ARS J. 30(6), 565–566 (1960)
10.
Loh, W.H.T.: Dynamics and Thermodynamics of Planetary Entry. Prentice Hall, Englewood Cliffs (1963a)
11.
Loh, W.H.T.: Some exact analytical solutions of planetary entry. AIAA J. 1(4), 836–842 (1963b)CrossRef
12.
Cohen, M. Some Closed Form Solutions to the Problem of Re-entry of Lifting and Non-lifting Vehicles//2nd Aerospace Sciences Meeting. New York, p. 46. (1965)
13.
Nyland, F.S. Hypersonic turning with constant bank angle control. The RAND Corporation. (1965)
14.
Bell, R.N. A closed-form solution to lifting reentry. Defense Technical Information Center. (1965)
15.
Chen, S.Y. The longitudinal and lateral range of hypersonic glide vehicles with constant bank angle. The RAND Corporation. (1966)
16.
Yu, W., Chen, W.: Entry guidance with real-time planning of reference based on analytical solutions. Adv. Space Res. 55(9), 2325–2345 (2015b)CrossRef
17.
Hanson, J.M., Coughlin, D.J., Dukeman, G. et al. Ascent, Transition, Entry, and Abort Guidance Algorithm Design for the X-33 Vehicle//Guidance, Navigation, and Control Conference and Exhibit. Boston. 4409 (1998)
18.
Mease, K.D., Chen, D.T., Teufel, P., et al.: Reduced-order entry trajectory planning for acceleration guidance. J. Guidance, Control, Dyn. 25(2), 257–266 (2002)CrossRef
19.
Dukeman, G.A. Profile-following Entry Guidance Using Linear Quadratic Regulator Theory//AIAA Guidance, Navigation, and Control Conference and Exhibit. Monterey. 4457 (2002)
20.
Shen, Z., Lu, P.: On-board generation of three-dimensional constrained entry trajectories. J. Guidance, Control, Dyn. 26(1), 111–121 (2003)CrossRef
21.
Zhang, Y.L., Chen, K.J., Liu, L., et al.: Entry trajectory planning based on three-dimensional acceleration profile guidance. Aerosp. Sci. Technol. 48, 131–139 (2016)CrossRef
22.
Powell, R.W.: Six-degree-of-freedom guidance and control-entry analysis of the HL-20. J. Spacecraft Rockets 30(5), 537–542 (1993)CrossRef
23.
Graesslin, M.H., Telaar, J., Schottle, U.M.: Ascent and reentry guidance concept based on NLP-methods. Acta Astronaut. 55(3–9), 461–471 (2004)CrossRef
24.
Zimmerman, C., Dukeman, G., Hanson, J.: Automated method to compute orbital reentry trajectories with heating constraints. J. Guidance, Control, Dyn. 26(4), 523–529 (2003)CrossRef
25.
Xie, Y., Liu, L., Tang, G., et al.: Highly constrained entry trajectory generation. Acta Astronaut. 88, 44–60 (2013)CrossRef
26.
Zhao, J., Zhou, R.: Reentry trajectory optimization for hypersonic vehicle satisfying complex constraints. Chin. J. Aeronaut. 26(6), 1544–1553 (2013)CrossRef
27.
Xu, B., Wang, D., Sun, F., et al.: Direct neural discrete control of hypersonic flight vehicle. Nonlinear Dyn. 70(1), 269–278 (2012)MathSciNetCrossRef
28.
Bu, X., Wu, X., Zhu, F., et al.: Novel prescribed performance neural control of a flexible air-breathing hypersonic vehicle with unknown initial errors. ISA Trans. 59, 149–159 (2015)CrossRef
29.
Shao, X., Wang, H.: Active disturbance rejection based trajectory linearization control for hypersonic reentry vehicle with bounded uncertainties. ISA Trans. 54, 27–38 (2015)CrossRef
30.
Tian, B., Fan, W., Zong, Q.: Integrated guidance and control for reusable launch vehicle in reentry phase. Nonlinear Dyn. 80(1–2), 397–412 (2015)CrossRef
31.
Zhao, J., Zhou, R.: Pigeon-inspired optimization applied to constrained gliding trajectories. Nonlinear Dyn. 82(4), 1781–1795 (2015)MathSciNetCrossRef
32.
Lu, P.: Entry guidance: a unified method. J. Guidance, Control, Dyn. 37(3), 713–728 (2014)CrossRef
33.
Yu, W., Chen, W. Guidance Scheme for Glide Range Maximization of a Hypersonic Vehicle//AIAA Guidance, Navigation, and Control Conference. Portland. 6714 (2011)
34.
Kermode, A.C.: Mechanics of Flight, 11th edn. Prentice Hall, London (2006)MATH
35.
Hu, J., Li, J., Chen, W. Longitudinal Characteristics of Steady Glide Trajectory for Hypersonic Vehicle//IEEE International Conference on Control, Automation and Information Sciences. Changshu. 272–279 (2015)
36.
Chowdhary, G., Jategaonkar, R.: Aerodynamic parameter estimation from flight data applying extended and unscented Kalman filter. Aerosp. Sci. Technol. 14(2), 106–117 (2010)CrossRef
37.
Burden, R.L., Faires, J.D.: Numerical Analysis, 9th edn. Cengage Learning, Boston (2010)MATH
38.
Zarchan, P. Tactical and Strategic Missile Guidance, 5th ed. AIAA Progress in Aeronautics and Astronautics (2007)
39.
Kidiyarova, V.G., Tarasenko, D.A., Schereia, I.A. Influence of Longitudinal Variations of the Structure of the Temperature, Pressure and Wind Fields in the Stratosphere and Mesosphere of the Northern Hemisphere//16 th COSPAR Plenary Meeting. Konstanz. (1973)
40.
Zeilik, M.A., Gregory, S.A. Introductory Astronomy and Astrophysics, 4th ed. Saunders College Publishing (1998)
Metadata
Title
Omnidirectional Autonomous Reentry Guidance Based on 3-D Analytical Glide Formulae Considering Influence of Earth’s Rotation
Authors
Wanchun Chen
Hao Zhou
Wenbin Yu
Liang Yang
Copyright Year
2021
Publisher
Springer Singapore
Book
Steady Glide Dynamics and Guidance of Hypersonic Vehicle

Print ISBN: 978-981-15-8900-3

Electronic ISBN: 978-981-15-8901-0

Copyright Year: 2021

DOI
https://doi.org/10.1007/978-981-15-8901-0_13

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