Zobrazeno 1 - 10
of 46
pro vyhledávání: '"QuanCheng Li"'
Publikováno v:
IEEE Access, Vol 9, Pp 76738-76749 (2021)
Covariance analysis describing function technique is a conventional method to solve the performance analysis of the nonlinear missile guidance system. Aiming at the faultiness of covariance analysis describing function technique and its improved meth
Externí odkaz:
https://doaj.org/article/11e6a63260af48739ccbc080ba72d71b
Publikováno v:
Aerospace, Vol 10, Iss 1, p 86 (2023)
As defense technology develops, it is essential to study the pursuit–evasion (PE) game problem in hypersonic vehicles, especially in the situation where a head-on scenario is created. Under a head-on situation, the hypersonic vehicle’s speed adva
Externí odkaz:
https://doaj.org/article/53e223ab2ee7424290671af7db5dac48
Publikováno v:
Aerospace, Vol 9, Iss 11, p 710 (2022)
Given the limitations of escape maneuvers and decoy deployment of combat aircraft under missile attacks; active defense dramatically improves the survival chances by launching active defense missiles to intercept incoming missiles. Different from pre
Externí odkaz:
https://doaj.org/article/c3a1f26012f54e4d837cbfb35b5b7b42
Publikováno v:
IEEE Access, Vol 7, Pp 86205-86216 (2019)
This paper proposes a state prediction adaptive sliding mode (SPASM) control method for the remotely piloted system (RPS). With consideration of the time delay caused by the large transmission delay existing in the RPS, a prediction algorithm is prop
Externí odkaz:
https://doaj.org/article/8d5cc601a58941279c03228215a3431d
Publikováno v:
Aerospace, Vol 9, Iss 4, p 221 (2022)
Aimed at the poor performance of guidance algorithms designed based on a linearized model in active defense under large leading angle deviation, both-way and one-way cooperative sliding mode guidance algorithms based on the smooth nonsingular termina
Externí odkaz:
https://doaj.org/article/6841cdde8da54df981966762d905f07f
Publikováno v:
International Journal of Aerospace Engineering, Vol 2019 (2019)
For the problem of hypersonic target interception, a novel midcourse guidance method with terminal-angle constraint is proposed. Referring to the air-breathing and the boost-gliding hypersonic targets, flight characteristics and difficulties of inter
Externí odkaz:
https://doaj.org/article/33227982c3254fe1b137eff2ffd350f4
Publikováno v:
Laryngoscope Investigative Otolaryngology. Aug2022, Vol. 7 Issue 4, p1107-1112. 6p.
Publikováno v:
International Journal of Robust and Nonlinear Control. 33:1456-1478
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ecc3569a96662a3c02f218d46e74f43d
https://doi.org/10.1002/rnc.6458
https://doi.org/10.1002/rnc.6458
Publikováno v:
Proceedings of 2022 International Conference on Autonomous Unmanned Systems (ICAUS 2022) ISBN: 9789819904785
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::340c4805b748a9c35fe435b97f076cc9
https://doi.org/10.1007/978-981-99-0479-2_183
https://doi.org/10.1007/978-981-99-0479-2_183
Publikováno v:
IEEE Access, Vol 9, Pp 76738-76749 (2021)
Covariance analysis describing function technique is a conventional method to solve the performance analysis of the nonlinear missile guidance system. Aiming at the faultiness of covariance analysis describing function technique and its improved meth
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::76174fa61556ef21050e6fbd05c138c0
https://ieeexplore.ieee.org/document/9439453/
https://ieeexplore.ieee.org/document/9439453/