Zobrazeno 1 - 10
of 26
pro vyhledávání: '"Jikun Ye"'
Publikováno v:
IEEE Access, Vol 8, Pp 192021-192029 (2020)
In this paper, fractional-order calculus theory is used to investigate the geometric law for intercepting an agile target. In order to overcome the challenges presented by the divergence of line of sight rate (LOSR) of proportional navigation (PN), t
Externí odkaz:
https://doaj.org/article/8d068dd6cda44d7cad71131a308261e7
Publikováno v:
International Journal of Aerospace Engineering, Vol 2022 (2022)
In the terminal guidance phase of intercepting aerial target, a guidance law, satisfying impact angle constraint, acceleration constraint, and second-order dynamic characteristic of interceptor autopilot, is designed based on the prescribed performan
Externí odkaz:
https://doaj.org/article/a3633c2e54c341969cb1edc434e436f9
Publikováno v:
International Journal of Aerospace Engineering, Vol 2021 (2021)
This paper presents a noncertainty equivalent adaptive backstepping control scheme for advanced fighter attitude tracking, in which unsteady effects, parameter uncertainties, and input constraints are all considered which increase the design difficul
Externí odkaz:
https://doaj.org/article/fe07e0c90cc34c4083d50fcb295d488b
Publikováno v:
International Journal of Aerospace Engineering, Vol 2019 (2019)
This paper investigates the problem of precise and quick tracking for gyrostabilized platform (GSP) with unknown hysteresis, unknown control directions, and unknown compound disturbance. Firstly, the dynamic model of GSP is transformed into a strict
Externí odkaz:
https://doaj.org/article/04be33171add4311b57c973fe614a429
Publikováno v:
International Journal of Aerospace Engineering, Vol 2017 (2017)
Based on the theory of fractional order calculus (FOC), a novel extended proportional guidance (EPN) law for intercepting the maneuvering target is proposed. In the first part, considering the memory function and filter characteristic of FOC, the nov
Externí odkaz:
https://doaj.org/article/f9ba2c55ada746dfb66e28cb6063cde7
Publikováno v:
Sensors, Vol 18, Iss 9, p 2927 (2018)
This paper investigates the design of a missile seeker servo system combined with a guidance and control system. Firstly, a complete model containing a missile seeker servo system, missile guidance system, and missile control system (SGCS) was creati
Externí odkaz:
https://doaj.org/article/c5656d1779604c99bea5d6f0af04cdd8
Publikováno v:
Scientific and Social Research. 4:1-8
Considering theory-focused and relatively dull content of Theory of Missile Guidance and Control, and the low learning motivation and weak practical skills of the students, this paper describes the practice and experience of blended teaching reform i
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5ae23f1d1b4e9dd1e14b43f04f8417f3
https://doi.org/10.26689/ssr.v4i10.4396
https://doi.org/10.26689/ssr.v4i10.4396
Publikováno v:
IEEE Access, Vol 8, Pp 192021-192029 (2020)
In this paper, fractional-order calculus theory is used to investigate the geometric law for intercepting an agile target. In order to overcome the challenges presented by the divergence of line of sight rate (LOSR) of proportional navigation (PN), t
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::d20f80e784264b37a412ae2b3e435ee7
https://ieeexplore.ieee.org/document/9226535/
https://ieeexplore.ieee.org/document/9226535/
Publikováno v:
International Journal of Aerospace Engineering, Vol 2019 (2019)
This paper investigates the problem of precise and quick tracking for gyrostabilized platform (GSP) with unknown hysteresis, unknown control directions, and unknown compound disturbance. Firstly, the dynamic model of GSP is transformed into a strict
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::e69b0ec1919ffc1940ec18a12d2ddf93
https://doi.org/10.1155/2019/2030617
https://doi.org/10.1155/2019/2030617
Publikováno v:
International Journal of Aerospace Engineering, Vol 2021 (2021)
This paper presents a noncertainty equivalent adaptive backstepping control scheme for advanced fighter attitude tracking, in which unsteady effects, parameter uncertainties, and input constraints are all considered which increase the design difficul
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::a8b40b0284057837f3a0c6d375fe5533
https://doaj.org/article/fe07e0c90cc34c4083d50fcb295d488b
https://doaj.org/article/fe07e0c90cc34c4083d50fcb295d488b