@inproceedings{739f57cc3f8142eebb76dbb2a0e28ace,
title = "The Impact angle guidance law Parameter design strategy Consider final speed constraint",
abstract = "This note studies the problem of impact falling angle guidance by considering the terminal speed constraint and proposes a new guidance parameter design strategy based on the law of falling angle guidance that adapts to the terminal speed is proposed. To this end, firstly, the general form of the extended trajectory shaping guidance law was deduced, and the non-dimensional acceleration characteristics of the guidance law were analyzed. Then, based on this, the influence of the change of the guidance law parameters on the dimensionless maneuvering energy is studied. A strategy for adjusting the guidance law parameters based on the end flight speed prediction results is proposed to satisfy the end speed constraints. Finally, the effectiveness of this strategy is verified by nonlinear ballistic simulation.",
keywords = "terminal velocity, the law of trajectory shaping guidance, velocity control",
author = "Lee, \{Bo Ya\} and Qiuqiu Wen and Guanqun Zhou",
note = "Publisher Copyright: {\textcopyright} 2018 IEEE.; 2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018 ; Conference date: 10-08-2018 Through 12-08-2018",
year = "2018",
month = aug,
doi = "10.1109/GNCC42960.2018.9018701",
language = "English",
series = "2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018",
publisher = "Institute of Electrical and Electronics Engineers Inc.",
booktitle = "2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018",
address = "United States",
}