1 |
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.
|
2 |
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.
|
3 |
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.
|
4 |
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.
DOI
|
5 |
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.
DOI
|
6 |
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.
DOI
|
7 |
Benson, D., A Gauss Pseudospectral Transcription for Optimal Control, Massachusetts Institute of Technology, 2005.
|
8 |
Garg, D., W. Hager, and A. Rao, Gauss Pseudospectral Method for Solving Infinite-Horizon Optimal Control Problems. 2010.
|
9 |
Andrews, D.G., An Introduction of Atmospheric Physics.
|
10 |
He, L., Solid Ballistic Missiles Design, Beihang University (BUAA)Press, 2004.
|
11 |
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.
DOI
|
12 |
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.
DOI
|
13 |
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.
DOI
|
14 |
Smith, I.E., General Formulation of the Iterative Guidance Mode. 1966.
|
15 |
Cherry, G., A general, explicit, optimizing guidance law for rocket-propelled spaceflight. 1964.
|
16 |
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.
DOI
|
17 |
Jaggers, R.F., An explicit solution to the exoatmospheric powered flight guidance and trajectory optimization problem for rocket propelled vehicles. 1977.
|
18 |
W, S., The Space Shuttle ascent guidance and control, in Guidance and Control Conference. American Institute of Aeronautics and Astronautics.1982.
|
19 |
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.
DOI
|
20 |
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.
|
21 |
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.
|
22 |
Zhou, H., T. Rahman, and W. Chen, "Neural network assisted inverse dynamic guidance for terminally constrained entry flight", ScientificWorldJournal, 2014. 2014: pp. 686040.
|
23 |
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.
|
24 |
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.
|