Based on the battery charging and discharging regulator (BCDR) in spacecraft power conditioning unit application, a bidirectional DC-DC converter BCDR with high direction-changing frequency is proposed in this paper, ...
详细信息
Based on the battery charging and discharging regulator (BCDR) in spacecraft power conditioning unit application, a bidirectional DC-DC converter BCDR with high direction-changing frequency is proposed in this paper, including the Weinberg-buck bidirectional DC-DC topology and the corresponding bidirectional control. Additionally, the test on the BCDR prototype shows that BCDR parallel modules could achieve the quick switching between charging and discharging with the direction-changing frequency meeting the requirement of 1 kHz, the regulated power bus of small voltage ripple, and high charging and discharging efficiency, in agreement with the expected design.
Optimal power management of shipboard power system for failure mode (OPMSF) is a significant and challenging problem considering the safety of system and person. Many existing works focused on the transient-time recov...
详细信息
One of the key subsystems from point of view of security of the complex IoT system is the smart business center (SB?) system. Some problems the design and operation of the SBC system are analyzed. When analysis of saf...
详细信息
The main characteristic of FroBot is the dual-swing-legs propulsion mechanism, and it is necessary for us to conduct a series of experiments to study its propulsion model, both on land and underwater. As the propulsio...
详细信息
作者:
Ritchie, PaulKarabacak, ÖzkanSieber, JanEarth System Science
College of Life and Environmental Sciences University of Exeter Harrison Building ExeterEX4 4QF United Kingdom Department of Electronic Systems
Automation and Control Aalborg University Fredrik Bajers Vej 7 C Aalborg East9220 Denmark Centre for Systems
Dynamics and Control College of Engineering Mathematics and Physical Sciences University of Exeter Harrison Building ExeterEX4 4QF United Kingdom
A classical scenario for tipping is that a dynamical system experiences a slow parameter drift across a fold tipping point, caused by a run-away positive feedback loop. We study what happens if one turns around after ...
详细信息
Nowadays wind turbine rotors are usually employed with pitch control mechanisms to avoid deep stall conditions. Despite that, wind turbines often operate under pitch fault situation causing massive flow separation to ...
Nowadays wind turbine rotors are usually employed with pitch control mechanisms to avoid deep stall conditions. Despite that, wind turbines often operate under pitch fault situation causing massive flow separation to occur. Pure Blade Element Momentum (BEM) approaches are not designed for this situation and inaccurate load predictions are already expected. In the present studies, BEM predictions are improved through the inclusion of a stall delay model for a wind turbine rotor operating under pitch fault situation of -2.3° towards stall. The accuracy of the stall delay model is assessed by comparing the results with available Computational Fluid Dynamics (CFD) simulations data.
This paper presents the system works,solution of the limited hydraulic source with the velocity inner loop,and the system optimal design method of reduction *** modeling and simplifying the system,the static and dynam...
详细信息
This paper presents the system works,solution of the limited hydraulic source with the velocity inner loop,and the system optimal design method of reduction *** modeling and simplifying the system,the static and dynamic characteristics are analyzed,and the selecting requirements of affecting its parameters are proposed.A method is raised to reduce the peak pressure of the hydraulic drive unit(PDU) inlet and outlet pipes and its internal motor.
This paper introduced a type of aircraft electric hydraulic pump system working principle,the key points of the system are analyzed and described,including calculation of boost pressure,system oil temperature control ...
详细信息
This paper introduced a type of aircraft electric hydraulic pump system working principle,the key points of the system are analyzed and described,including calculation of boost pressure,system oil temperature control design,environmental temperature checking,starting logic design,the system validation and verification methods are *** system passed through the ground test and flight time Validation,and worked well and reliably.
Article deals with research problem of controlsystem for damping object oscillations using active hydro bearing functioning. With the simulation the behavior of the system in the presence of various external harmonic...
详细信息
ISBN:
(纸本)9781467383844
Article deals with research problem of controlsystem for damping object oscillations using active hydro bearing functioning. With the simulation the behavior of the system in the presence of various external harmonic perturbations with a variable amplitude and frequency is studied.
For a priori undetermined nonlinear multi-mode dynamic object with several statement delays and the relative order greater than one, it offers a combined adaptive controlsystem, synthesized using the hyperstability c...
详细信息
ISBN:
(纸本)9781467383844
For a priori undetermined nonlinear multi-mode dynamic object with several statement delays and the relative order greater than one, it offers a combined adaptive controlsystem, synthesized using the hyperstability criterion and L-dissipativity conditions.
暂无评论