Zobrazeno 1 - 4
of 4
pro vyhledávání: '"David C. Foreman"'
Publikováno v:
AIAA Guidance, Navigation, and Control Conference.
In this paper, we use Higher-Order Sliding Mode (HOSM) control to perform trajectory shaping for non-line-of-sight delivery of a mortar round that has been fitted with a single canard. To minimize cost and maximize ease of use, no gyroscope or accele
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::637096ebb3a1bf2035fe4954b2daf025
https://doi.org/10.2514/6.2011-6709
https://doi.org/10.2514/6.2011-6709
This chapter presents a Higher Order Sliding Mode (HOSM) Control for automatic docking between two space vehicles. The problem considered requires controlling the vehicles’ relative position and relative attitude. This type of problem is generally
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c591be0fac49f0ff2706e3bb65c3b99a
https://doi.org/10.5772/15801
https://doi.org/10.5772/15801
Publikováno v:
AIAA Guidance, Navigation, and Control Conference.
Novel options are presented for the control of a high-endo/low-exo interceptor missile during its boost and midcourse flight phases. For boost, we use third-order quasicontinuous Higher-Order Sliding Mode (HOSM) control and second-order HOSM differen
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7eae3ea01396e9e610bb6b2c110cbcf6
https://doi.org/10.2514/6.2010-7579
https://doi.org/10.2514/6.2010-7579
Publikováno v:
ACC
An integrated autopilot-and-guidance algorithm that is robust to missile's model parametric and dynamic uncertainties is developed, using Higher Order Sliding Mode (HOSM) quasi-continuous control, for an endoatmospheric missile. Unlike in traditional
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::be94245beceb2a432c4ad76fc511c8d3
https://doi.org/10.1109/vss.2010.5544652
https://doi.org/10.1109/vss.2010.5544652