참고문헌
- Smith, I.E., General Formulation of the Iterative Guidance Mode. 1966.
- Cherry, G., A general, explicit, optimizing guidance law for rocket-propelled spaceflight. 1964.
- Jaggers, R.F., An explicit solution to the exoatmospheric powered flight guidance and trajectory optimization problem for rocket propelled vehicles. 1977.
- W, S., The Space Shuttle ascent guidance and control, in Guidance and Control Conference. American Institute of Aeronautics and Astronautics.1982.
- Jezewski, D.J., "An optimal, analytic solution to the linear-gravity, constant-thrust trajectory problem", Journal of Spacecraft and Rockets,Vol. 8, No. 7, 1971, pp. 793-796. https://doi.org/10.2514/3.30320
- Lu, P., et al., "Rapid Optimal Multiburn Ascent Planning and Guidance", Journal of Guidance, Control, and Dynamics, Vol. 31, No. 6, 2008, pp. 1656-1664. https://doi.org/10.2514/1.36084
- Ping, L., Z. Lijun. and S. Hongsheng, Ascent Guidance for Responsive Launch: A Fixed-Point Approach, in AIAA Guidance, Navigation, and Control Conference and Exhibit, American Institute of Aeronautics and Astronautics, 2005.
- Lu, P. and J. Samsundar, "Closed form solutions of constrained trajectories application in optimal ascent of aerospace plane", in AIAA International Aerospace Planes Conference, AIAA: Orlando, FL, 1992.
- Zhou, H., T. Rahman, and W. Chen, "Neural network assisted inverse dynamic guidance for terminally constrained entry flight", ScientificWorldJournal, 2014. 2014: pp. 686040.
- Zhou, H., et al., "Onboard pseudospectral guidance for re-entry vehicle", Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2013.
- Rose, M.B. and D. Geller, "Linear Covariance Techniques for Powered Ascent", in AIAA Guidance, Navigation, and Control Conference, Americal Institute of Aeronautics and Astronautics: Toronto, Ontario Canada, 2010.
- Greg, D., "Atmospheric Ascent Guidance for Rocket- Powered Launch Vehicles", in AIAA Guidance, Navigation, and Control Conference and Exhibit, American Institute of Aeronautics and Astronautics, 2002.
- Dukeman, G. and A. Calise, "Enhancements to an Atmospheric Ascent Guidance Algorithm", in AIAA Guidance, Navigation, and Control Conference and Exhibit, AIAA: Austin, Texas, 2003.
- Lu, P., S. Forbes, and M. Baldwin, "A Versatile Powered Guidance Algorithm", in AIAA Guidance, Navigation, and Control Conference, American Institute of Aeronautics and Astronautics: Minneapolis, Minnesota, 2012.
- Lu, P. and B. Pan, "Highly Constrained Optimal Launch Ascent Guidance", Journal of Guidance, Control, and Dynamics, Vol. 33, No. 2, 2010, pp. 404-414. https://doi.org/10.2514/1.45632
- Zhang, L. and P. Lu, "Fixed-point algorithms for optimal ascent trajectories of launch vehicles", Engineering Optimization, Vol. 40, No. 4, 2008, pp. 361-381. https://doi.org/10.1080/03052150701732566
- Yang, L., H. Zhou, and W. Chen, "Application of linear gauss pseudospectral method in model predictive control", Acta Astronautica, Vol. 96, 2014, pp. 175-187. https://doi.org/10.1016/j.actaastro.2013.11.038
- Benson, D., A Gauss Pseudospectral Transcription for Optimal Control, Massachusetts Institute of Technology, 2005.
- Garg, D., W. Hager, and A. Rao, Gauss Pseudospectral Method for Solving Infinite-Horizon Optimal Control Problems. 2010.
- Andrews, D.G., An Introduction of Atmospheric Physics.
- He, L., Solid Ballistic Missiles Design, Beihang University (BUAA)Press, 2004.
- Boskovic, J.D., et al., "Multiple-Model Adaptive Fault-Tolerant Control of a Planetary Lander", Journal of Guidance, Control, and Dynamics, Vol. 32, No. 6, 2009, pp. 1812-1826. https://doi.org/10.2514/1.42719
- Boskovic, J.D., S. Bergstrom, and R.K. Mehra, "Robust Integrated Flight Control Design Under Failures, Damage, and State-Dependent Disturbances", Journal of Guidance, Control, and Dynamics, Vol. 28, No. 5, 2005, pp. 902-917. https://doi.org/10.2514/1.11272
- Hanson, J., A.D. Hill, and B.B. Beard, "Launch Vehicle Abort Analysis of Failures Leading to Loss of Control", Journal of Spacecraft and Rockets, Vol. 49, No. 5, 2012, pp. 925-934. https://doi.org/10.2514/1.A32061
피인용 문헌
- Waypoints Following Guidance for Surface-to-Surface Missiles vol.19, pp.1, 2018, https://doi.org/10.1007/s42405-018-0007-5
- Tracking Control of Hypersonic Vehicles with Input Saturation Based on Fast Terminal Sliding Mode pp.2093-2480, 2019, https://doi.org/10.1007/s42405-018-0109-0