Dynamic guidance of orbiter gliders: alignment, final approach, and landing

Author:

Fonseca João,Dilão RuiORCID

Publisher

Springer Science and Business Media LLC

Subject

Space and Planetary Science,Aerospace Engineering

Reference23 articles.

1. Barton, G.H., Grubler, A.C., Dyckman, T.R.: New methodologies for onboard generation of TAEM trajectories for autonomous RLVs. In: Core Technologies for Space Systems Conference. https://pdfs.semanticscholar.org/a327/e02cfeacf89cd37ae5f18011df6d72dcfc03.pdf (2002)

2. Bernot, P.T.: Aerodynamic Characteristics of the 140A/B Space Shuttle Orbiter at Mach 10.3, NASA Technical Memorandum 80086. https://ntrs.nasa.gov/search.jsp?R=19790014013 (1979)

3. Chern, J.S., Vihn, N.X.: Optimum Reentry Trajectories of a Lifting Vehicle, NASA Contractor Report 3236. https://ntrs.nasa.gov/search.jsp?R=19800007820 (1980)

4. Dilão, R., Fonseca, J.: Dynamic trajectory control of gliders. In: Chu, Q., Mulder, B., Choukroun, D., van Kampen, E.J., de Visser, C., Looye, G. (eds) Advances in Aerospace Guidance, Navigation and Control, Selected Papers of the 2nd CEAS Specialist Conference on Guidance, Navigation and Control, pp. 373–386. Springer, Berlin, Heidelberg (2013)

5. Dilão, R., Fonseca, J.: Dynamic guidance of gliders in planetary atmospheres. J. Aerosp. Eng. 29(1), 04015012 (2016). https://doi.org/10.1061/(ASCE)AS.1943-5525.0000499

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