Results 41 to 50 of about 1,519 (231)

Fractional-Order Sliding Mode Guidance Law for Intercepting Hypersonic Vehicles

open access: yesAerospace, 2022
This paper addresses the problem of a low-speed missile intercepting a hypersonic vehicle in the longitudinal plane. Firstly, based on the concept of the zero of the angular rate of the line-of-sight (LOS) angle, the guidance system is established by ...
Shuangxi Liu   +4 more
doaj   +1 more source

Design Challenges to Expand the Functionality of Drones: Deformable Rotorcraft and Nature‐Inspired Flapping Drones

open access: yesAdvanced Intelligent Systems, EarlyView.
This review systematically analyzes deformable drones, including extendable, foldable, and tilting configurations, along with nature‐inspired flapping rotorcraft. By classifying deformation principles and structural mechanisms, design trade‐offs, functional capabilities, and future development potential are highlighted.
Ju‐Hee Lee   +9 more
wiley   +1 more source

Impact-Time-Control Guidance Law for Hypersonic Missiles in Terminal Phase

open access: yesIEEE Access, 2020
Recent researches on hypersonic vehicles adopted in military have gained a lot of interest because of its high flight speed and efficiency. However the guidance laws for hypersonic missiles against the anti-missile system to increase survivability and ...
Chenhao Zhu   +4 more
doaj   +1 more source

Harnessing Carbon‐Containing Materials for Next‐Generation High‐Temperature Electromagnetic Wave Absorbers

open access: yesCarbon Energy, EarlyView.
Traditional carbon materials show limited high‐temperature oxidation resistance, which becomes pronounced above 673 K and significantly restricts their practical applicability. To address this challenge, enhancing polarization loss and leveraging its negative temperature dependence to offset the temperature‐induced increase in conductance loss are ...
Yang Li   +9 more
wiley   +1 more source

An examination of high-speed aircraft – Part 2: Safety and reliability

open access: yesTransportation Engineering
This paper presents a detailed accident investigation into incidents involving high-speed vehicles, particularly supersonic and hypersonic platforms.
Luke Pollock, Graham Wild
doaj   +1 more source

Composition‐Dependent Wide‐Range Tunability of Optical and Electronic Properties in SnSxSe(2‐x) Alloy Nanosheets

open access: yesSmall, EarlyView.
A scalable, solution‐processed route unlocks the full SnSxSe(2–x) alloy spectrum, delivering finely tunable optical and electronic properties—from metallic‐like SnSe2 to wide‐bandgap SnS2. Composition‐guided control over in‐ and out‐of‐plane transport enables performance‐optimized photoelectrochemistry, charting a versatile roadmap for designer ...
Nicolas J. Diercks   +12 more
wiley   +1 more source

Research Status and Development of Adaptive Control Technology for Hypersonic Aircraft [PDF]

open access: yesHangkong bingqi
The future war presents a development trend of “intelligence and multidimensionality”, and conventional control technology is difficult to adapt to wide speed range flight conditions.
Tao Yixuan, Li Zihao, Huang Wei
doaj   +1 more source

Collaborating in future states—Contextual instability, paradigmatic remaking, and public policy

open access: yesAustralian Journal of Public Administration, EarlyView.
Abstract Collaboration is ubiquitous in public policy life, with its presence and profile determined by prevailing governance conditions. Commitments to globalisation and marketisation in the latter part of the 20th century marked the onset of an era defined by collaboration, between and across tiers and spheres of government, with non‐state actors ...
Helen Sullivan
wiley   +1 more source

Numerical Analysis of the Interference Effect of Oblique Forward Jet on the Rear Body of Aircraft in Extreme Environments

open access: yes气体物理
The oblique forward jet from the rear body serves as an effective mechanism for achieving rapid separation between the front and rear stages of an aircraft.
Yang WANG, Xinyu SONG, Shengyi WANG
doaj   +1 more source

Study on Ground Experimental Method of Stagnation Point Large Heat Flux of Typical Sharp Wedge Leading Edge Structure

open access: yesAerospace, 2023
In this paper, aimed at the problem of large temperature gradient thermal testing with the typical sharp wedge leading edge structure of a hypersonic vehicle, a subsonic high-temperature combustion gas heating (SHCH) test device is used to conduct a ...
Ri Wang   +5 more
doaj   +1 more source

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