Results 21 to 30 of about 539,000 (325)

Synthesis of Suboptimal Guidance Law for Anti-Tank Guided Missile with Terminal Impact Angle Constraint Based on the SDRE Technique

open access: yesArchives of Advanced Engineering Science, 2023
In this paper, the homing-phase guidance law is proposed against a stationary target in the planar engagement scenario. In this problem, two technical criteria that the guidance law must achieve are: first, zero terminal miss distance, and second ...
Van Hai Tran   +4 more
semanticscholar   +1 more source

$\mathcal N=2$ Supersymmetry Deformations, Electromagnetic Duality and Dirac-Born-Infeld Actions [PDF]

open access: yes, 2019
We study the general deformation of $\mathcal N=2$ supersymmetry transformations of a vector multiplet that forms a (constant) triplet under the $SU(2)$ R-symmetry corresponding to the magnetic dual of the triplet of the Fayet-Iliopoulos (FI) parameters.
Antoniadis, Ignatios   +2 more
core   +4 more sources

Opaque Branes in Warped Backgrounds [PDF]

open access: yes, 2002
We examine localized kinetic terms for gauge fields which can propagate into compact, warped extra dimensions. We show that these terms can have a relevant impact on the values of the Kaluza-Klein (KK) gauge field masses, wave functions, and couplings to
A. Lewandowski   +34 more
core   +2 more sources

Guidance law with impact time and impact angle constraints

open access: yesChinese Journal of Aeronautics, 2013
AbstractA novel closed-form guidance law with impact time and impact angle constraints is proposed for salvo attack of anti-ship missiles, which employs missile’s normal acceleration (not jerk) as the control command directly. Firstly, the impact time control problem is formulated as tracking the designated time-to-go (the difference between the ...
Zhang, Youan, Ma, Guoxin, Liu, Aili
openaire   +1 more source

Cubature Kalman Filters Model Predictive Static Programming Guidance Method with Impact Time and Angle Constraints Considering Modeling Errors

open access: yesMathematics, 2023
This paper proposes a CKF-MPSP guidance method for hitting stationary targets with impact time and angle constraints for missiles in the presence of modeling errors.
Zihan Xie   +3 more
doaj   +1 more source

Direct Feedback Alignment with Sparse Connections for Local Learning [PDF]

open access: yes, 2019
Recent advances in deep neural networks (DNNs) owe their success to training algorithms that use backpropagation and gradient-descent. Backpropagation, while highly effective on von Neumann architectures, becomes inefficient when scaling to large ...
Crafton, Brian   +3 more
core   +2 more sources

Impact Angle Control Guidance Law Considering the Seeker’s Field-of-View Constraint Applied to Variable Speed Missiles

open access: yesIEEE Access, 2020
Recently, multiple constraints have been considered in the design of guidance laws. Most of the existing impact angle control guidance laws considering the seeker's field-of-view constraint are only applicable to constant speed missiles and have other ...
Shou Zhou   +3 more
doaj   +1 more source

Novel Particle Swarm Optimization Guidance for Hypersonic Target Interception with Impact Angle Constraint

open access: yesInternational Journal of Aerospace Engineering, 2022
Considering that the terminal impact angle constraint can improve the interception performance of hypersonic target, a novel particle swarm optimization guidance (NPSOG) algorithm is proposed to satisfy the impact angle constraint.
Fan He, Weiyi Chen, Yang Bao
doaj   +1 more source

Analysis of Line-of-Sight Angle Characteristics for Intercepting a Non-Maneuvering Target With Impact Angle Constraints

open access: yesIEEE Access, 2023
With the widespread informationization in modern warfare, higher requirements are required for monitoring the high-value target’s movement state and the corresponding attack conditions.
Xin Sun   +5 more
doaj   +1 more source

Research on Cooperative Guidance Law of Multi-Missile Based on Trajectory Super-Real Time Simulation [PDF]

open access: yesHangkong bingqi, 2021
It is very difficult to conduct time cooperation guidance of multi-missile when the velocity of missile is uncontrollable. Based on the trajectory super real-time simulation method, which can gives out time-to-go exactly as well as future trajectory ...
Zhang Peng, Lu Hao, Shen Xin
doaj   +1 more source

Home - About - Disclaimer - Privacy