Zobrazeno 1 - 10
of 163
pro vyhledávání: '"Honghao Yue"'
Publikováno v:
Actuators, Vol 13, Iss 9, p 343 (2024)
Unmanned Aerial Vehicle (UAV) aerial recovery is a challenging task due to the limited maneuverability of both the transport aircraft and the UAV, making it difficult to establish an effective capture connection in the airflow field. In previous stud
Externí odkaz:
https://doaj.org/article/a0e3de10c532491dbf0e165b89a66506
Publikováno v:
Aerospace, Vol 11, Iss 5, p 394 (2024)
For future large-scale CubeSat applications in orbit, the deployer must accommodate a greater number of CubeSats and facilitate cluster releases. This paper introduces an improved A* algorithm tailored for CubeSat in-orbit transfer path planning. Unl
Externí odkaz:
https://doaj.org/article/0a159f470a584a328ed649d72c7d632b
Publikováno v:
Biomimetics, Vol 9, Iss 2, p 111 (2024)
Aerial recovery and redeployment can effectively increase the operating radius and the endurance of unmanned aerial vehicles (UAVs). However, the challenge lies in the effect of the aerodynamic force on the recovery system, and the existing road-base
Externí odkaz:
https://doaj.org/article/904fc19c623244a0a5108fc223213da3
Publikováno v:
Sensors, Vol 23, Iss 20, p 8577 (2023)
This paper reports a method for calculating the electromagnetic force acting on an aluminum honeycomb sandwich panel moving in a magnetic field. This research is motivated by the non-contact electromagnetic detumbling technology for space non-coopera
Externí odkaz:
https://doaj.org/article/adfc5d48c3ed48f3bafc2317c25a1a57
Publikováno v:
Aerospace, Vol 10, Iss 10, p 844 (2023)
In this paper, a morphing aircraft with a deployable flared skirt is proposed, and the influence of the flare skirt on the static stability of hypersonic aircraft is studied. The theoretical model of static stability of slender aircraft is establishe
Externí odkaz:
https://doaj.org/article/d5e5da43446d4e449dc962e6869c0e9f
Publikováno v:
Advances in Mechanical Engineering, Vol 14 (2022)
In this paper, based on the development of the non-pyrotechnic low impact connection and separation device for heavy load connection of large space vehicles, the design method of connection and separation device is studied. The traditional heavy load
Externí odkaz:
https://doaj.org/article/c35e071c316c40e990c1c6712465be23
Publikováno v:
Metals, Vol 13, Iss 5, p 881 (2023)
This report is on convolution neural network (CNN) fusion lock-in thermography, which can implement the intelligent identification of defects for aviation honeycomb sandwich composites (HSCs). First, HSCs specimens with subsurface delamination defect
Externí odkaz:
https://doaj.org/article/259b95a0ee9c45488d9acdc320f96995
Publikováno v:
IEEE Access, Vol 8, Pp 122304-122313 (2020)
This article proposes a novel soft pneumatic actuator inspired by the segmented structure of earthworms. The actuator adopts a new structure of free bottom to eliminate the constraint of the bottom and enlarge the bending capacity of the actuator. Th
Externí odkaz:
https://doaj.org/article/94ab3f18afd14e5cb3eec262c3b1ec19
Publikováno v:
International Journal of Smart and Nano Materials, Vol 11, Iss 1, Pp 65-77 (2020)
After the satellite is launched with the carrier rocket, it is necessary to separate the satellite from the rocket at an appropriate time to ensure that the satellite enters the intended orbit. In this process, it is vital to ensure a reliable connec
Externí odkaz:
https://doaj.org/article/5a025beabf534a63a464c7f5c355f83e
Publikováno v:
Aerospace, Vol 9, Iss 12, p 794 (2022)
Due to the super flexibility and strong nonlinearity of space membrane antennas, the dynamic response of a space membrane antenna will be affected by the rigid–flexible coupling effect in the process of orbital maneuvering. In this case, the dynami
Externí odkaz:
https://doaj.org/article/43086b72975143a08373423cd7ce4536