Open Access
| Issue |
Volume 10, 2018
Progress in Flight Dynamics, Guidance, Navigation, and Control – Volume 10
|
|
|---|---|---|
| Page(s) | 105 - 120 | |
| DOI | https://doi.org/10.1051/eucass/201810105 | |
| Published online | 08 June 2018 | |
- Jeremy, R.R., and R.R. Zachry. 2007. A comparison of two Orion skip entry guid- ance algorithms. AIAA Guidance, Navigation and Control Conference and Exhibit. 19 p. [Google Scholar]
- Bairstow, S.H., and G.H. Barton. 2007. Orion reentry guidance with extended range capability using PredGuid. AIAA Guidance, Navigation and Control Con- ference and Exhibit. 17 p. [Google Scholar]
- Putnam, Z.R., S.H. Bairstow, R.D. Braun, et al. 2008. Improving lunar return en-try range capability using enhanced skip trajectory guidance. J. Spacecraft Rockets 45:309–315. [NASA ADS] [CrossRef] [Google Scholar]
- Christopher,W.B., and L. Ping. 2008. Skip entry trajectory planning and guidance. J. Guid. Control Dynam. 31:1210–1219. [Google Scholar]
- Christopher, W. B., and L. Ping. 2010. Comparison of numerical predictor– corrector and Apollo skip entry guidance algorithms. AIAA Guidance, Navigation, and Control Conference. 20 p. [Google Scholar]
- Vernis, P., F. Spreng, and G. Gelly. 2011. Accurate skip-entry guidance for low to medium L/D spacecrafts return missions requiring high range capabilities. AIAA Guidance, Navigation, and Control Conference. 15 p. [Google Scholar]
- Ping, L. 2008. Predictor–corrector entry guidance for low-lifting vehicles. J. Guid. Control Dynam. 31:1067–1075. [Google Scholar]
- Moseley, P.E. 1969. The Apollo entry guidance: A review of the mathematical development and its operational characteristics. Huston, TX. TRW 69-FMT-791. [Google Scholar]
- De Nicola, D., and V. Antonio. 2010. Fully structured aerodynamic model for parameter identification of a reentry experimental vehicle. J. Spacecraft Rockets 47:113–124. [NASA ADS] [CrossRef] [Google Scholar]
- Gamble, J.D., C. J. Cerimele, T. E. Moore, and J. Higgins. 1988. Atmospheric guidance concepts for an aeroassisted flight experiment. J. Astronaut. Sci. 36:45–71. [NASA ADS] [Google Scholar]
- Powell, R.W., and R.D. Braun. 1993. Six-degree-of-freedom guidance and control analysis of Mars aerocapture. J. Guid. Control Dynam. 16:1038–1044. [NASA ADS] [CrossRef] [Google Scholar]
- Evans, S.W., and G.A. Dukeman. 1995. Examination of a practical aerobraking guidance algorithm. J. Guid. Control Dynam. 18:471–477. [NASA ADS] [CrossRef] [Google Scholar]
- Bairstow, S.H. 2006. Reentry guidance with extended range capability for low L/D spacecraft. Cambridge, MA: Department of Aeronautics and Astronautics, Massachusetts Institute of Technology. M.S. Thesis. [Google Scholar]
- Zarchan, P., and H. Musoff. 2005. Fading memory filter. Ch. 15. Fundamentals of Kalman filtering: A practical approach. 2nd ed. Progress in astronautics and aeronautics ser. Reston, VA: AIAA. 208:647–676. [Google Scholar]