China Aerospace Science and Industry Corporation (CASIC) - Extended optimal guidance law with impact angle and acceleration constriants

Author(s): Ran Li ; Qunli Xia ; Qiuqiu Wen
Publisher: China Aerospace Science and Industry Corporation (CASIC)
Publication Date: 1 October 2014
Volume: 25
Page(s): 868 - 876
ISSN (Electronic): 1004-4132
DOI: 10.1109/JSEE.2014.00100
Regular:

The extended optimal guidance law with terminal constraints of miss distance and impact angle is derived by the Schwartz inequality. To reduce terminal acceleration and eliminate gravity... View More

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