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A novel design for a radial field switching reluctance motor with a sandwich-type C-core architecture is proposed. This approach combines elements of both traditional axial and radial field distribution techniques. This motor, similar to an in-wheel construction, is mounted on a shared shaft and is simple to operate and maintain. The rotor is positioned between the two stators in this configuration. The cores and poles of the two stators are separated from one another both magnetically and electrically. Both stators can work together or separately to produce the necessary torque. This adds novelty and improves the design’s suitability for use with electrical vehicles (EVs). A good, broad, and adaptable torque profile is provided by this setup at a modest excitation current. This work presents the entire C-core radial field switched reluctance motor (SRM) design process, including the computation of motor parameters through computer-aided design (CAD). The CAD outputs are verified via
Patel, Nikunj R.Mokariya, Kashyap L.Chavda, Jiten K.Patil, Surekha
ABSTRACT Route planning plays an integral role in mission planning for ground vehicle operations in urban areas. Determining the optimum path through an urban area is a well understood problem for traditional ground vehicles; however, in the case of autonomous unmanned ground vehicles (UGVs), additional factors must be considered. For a UGV, perception, rather than mobility, will be the limiting factor in determining operational areas. Current ground vehicle route planning techniques do not take perception concerns into account, and these techniques are not suited for route planning for UGVs. For this study, perception was incorporated into the route planning process by including expected sensor accuracy for GPS, LIDAR, and inertial sensors into the path planning algorithm. The path planner also accounts for additional factors related to UGV performance capabilities that affect autonomous navigation
Durst, Phillip J.Goodin, ChristopherSong, PeilinDu, Thien K.
ABSTRACT A methodology based on a combination of commercial software tools is developed for rendering complex acoustic scenes in real time. The methodology aims to bridge the gap between real time acoustic rendering algorithms which lack important physics for the exterior urban environment and more rigorous but computationally expensive geometric or wave-based acoustics software by incorporating pre-computed results into a real time framework. The methodology is developed by surveying the best in class commercial software, outlining a general means for accommodating results from each, and identifying areas where supplemental capability is required. This approach yields a real time solution with improved accuracy. Strengths and limitations in current commercial technologies are identified and summarized
Mattson, Steven GPolakowski, Stephen E.Pruetz, JeffSmith, RobJanicki, Phil
ABSTRACT The recent climate change plan for the United States Army states that hybridized combat vehicles will enter the fleet by 2050. The Bradley Fighting Vehicle (BFV) and its family of vehicles are prime candidates for hybridization. This paper sets out to perform a drive cycle analysis for the BFV using its traditional powertrain along with hybridized powertrains. The analysis considers both series and parallel hybrid architectures, where the size of the batteries are based on modifications to the existing powertrain. Three different drive cycles are considered – stationary, highway, and off-road. The model accounts for accelerative forces, transmission losses, cooling losses, drag, road grade, tractive losses, and ancillary equipment. The results indicate that both parallel and series hybrids provide reduced fuel consumption and increased range. Of the two, the series hybrid architecture provides more overall benefits. The study concludes by discussion of the technical challenges
Razon, CourtneyMittal, Vikram
ABSTRACT This paper discusses the development of a methodology to generate drive cycles having a finite duration, but which are statistically representative of a larger set of usage data collected from fleet vehicles operating in the field. Given field-generated time vs. velocity data, acceleration at each data point is calculated, and each velocity and acceleration pair is binned using some calibrated level of fidelity. As a result, a velocity-acceleration matrix representing each vehicle operating point, as well as cumulative probability distribution functions for acceleration change and take-off acceleration are generated. These cumulative distribution functions are utilized to pick random velocity-acceleration pairs from the corresponding matrix, and the concatenation of each consecutive chosen velocity-acceleration pair constitutes the final drive cycle. Three drive cycles representing the high-, medium- and low-speed operation of the vehicle are generated from the field data, and
Dagci, Oguz H.Cook, AndrewShaw, Phillip
With the rapid advancement in unmanned aerial vehicle (UAV) technology, the demand for stable and high-precision electro-optical (EO) pods, such as cameras, lidar sensors, and infrared imaging systems, has significantly increased. However, the inherent vibrations generated by the UAV’s propulsion system and aerodynamic disturbances pose significant challenges to the stability and accuracy of these payloads. To address this issue, this paper presents a study on the application of high-static low-dynamic stiffness (HSLDS) vibration isolation devices in EO payloads mounted on UAVs. The HSLDS system is designed to effectively isolate low-frequency and high-amplitude vibrations while maintaining high static stiffness, ensuring both stability during hovering and precise pointing capabilities. A nonlinear dynamic system model with two degrees of freedom is formulated for an EO pod supported by HSLDS isolators at both ends. The model’s natural frequencies are determined, and approximate
Tian, YishenGuo, GaofengWang, GuangzhaoWei, WanBao, LingcongDong, GuanLi, Liujie
This study proposes a multi-mode switching control strategy based on electromagnetic damper suspension (EMDS) to address the different performance requirements of suspension systems on variable road surfaces. The working modes of EMDS are divided into semi-active damping mode and energy harvest mode, and the proposed mode switching threshold is the weighted root mean square value of acceleration. For the semi-active damping mode, a controller based on LQR(Linear Quadratic Regulator) was designed, and a variable resistance circuit was also designed to meet the requirements of the semi-active mode, which optimized the damping effect relative to passive suspension. For the energy harvest mode, an energy harvest circuit was designed to recover vibration energy. In order to reduce the deterioration of suspension performance caused by frequent mode switching in the mode switching strategy, as frequent system switching can lead to system disorder, deterioration of damping effect, and
Zeng, ShengZhang, BangjiTan, BohuanQin, AnLai, JiewenWang, Shichen
This study leverages the temperature impact data obtained from the battery systems of airworthiness-certified fixed-wing electric aircraft to predict and correct the performance of eVTOL battery systems under various temperature conditions. Due to the lack of airworthiness-certified eVTOL models, it is challenging to directly test battery system parameters under temperature variations. However, using data from Ma Xin's team's production batteries tested on certified fixed-wing electric aircraft, we can accurately measure the effects of temperature changes. The capacity retention data at temperatures of -40°C, -20°C, -10°C, 0°C, 0°C, 25°C, 35°C, 45°C, 55°Care 78.14%, 83.3%, 84.1%, 88.1%, 92.3%, 100.0%, 102.0%, 103.9%, 104.6%. These quantified results provide a basis for modeling and experimental validation of eVTOL battery systems, ensuring their performance and safety across a wide range of temperatures. Although there are some research of battery system of eVtol in room temperature
Ma, XinDing, ShuitingPan, Yilun
Abstract This paper analyzes the system-level state of health (SOH) and its dependence on the SOHs of the battery modules within the battery system. Due to the stochastic nature of battery aging processes and their dependance on charge/discharge, depth, temperature, and environment conditions, prior or long-term prediction of each module’s SOH is difficult. Based on estimated SOHs of battery modules during battery operation, we demonstrate how the SOH of the entire system decays when battery modules age and become increasingly diversified in their maximum ampere-hour capacities. System-level energy efficiency is analyzed. It is shown that by using battery reconfiguration after a length of service, the overall battery usable capacities can be utilized more efficiently, leading to extended operational ranges of the battery system. Analysis methods and simulation studies are presented
Wang, Le YiYin, GeorgeDing, Yi
ABSTRACT This paper describes ongoing work to develop and validate an improved waveguide model in order to support analysis of shielding effectiveness at frequencies from 8 GHz to 25 GHz. Waveguides may be used in the coolant loop for liquid-cooled, high-voltage power electronics to maintain the shielding effectiveness of the enclosure surrounding the power electronics. Different formulas for shielding effectiveness are reviewed and their applicability and limitations examined. The improved model is then used to predict the shielding effectiveness of an air-filled waveguide with a hexagonal or “honeycomb” insert installed. The results obtained are then compared with results obtained by modeling and simulation using FEKO
Faust, Scott W.
ABSTRACT Rubber tracks are now extremely competitive for vehicles up to 50 tons and fully fielded on 39 ton vehicles. They represent the best of what technology can offer for tracked vehicles, in terms of high durability, performance and low life cycle cost. This is mainly attributed to the optimization through the five (5) technological tools described in this paper. Better from its numerous distinctive advantages, rubber tracks can be adapted to suit virtually any specific need. This ductile rubber track technology can be shaped to match today’s requirements, with the help of advanced rubber compounding and computer simulations
Marcotte, Tommy
ABSTRACT With the development of the next generation of military vehicles, the demand for significant amounts of electrical power is increasing, making the design of electrical machines, such as the vehicle alternator, integral to the powertrain design. This shows the importance of the machines’ size and efficiency, and the great influence they will have on the vehicle powertrain design process. In this paper, a finite-element-based scaling technique, capable of quickly generating torque-speed curves and efficiency maps for new machine designs, is improved to have two dimensional scaling factors instead of scaling the dimensions uniformly, thus increasing the flexibility of the tool. First, a magnetostatic finite-element-analysis (FEA) is conducted on a base machine, producing data such as torque, flux linkage, and demagnetizing field intensity in the permanent magnets, over a wide range of current magnitudes and phase angles. Then, based on the dimensional and winding scaling factors
Wang, YuanyingHofmann, HeathIvanco, AndrejRizzo, Denise
ABSTRACT Ground vehicle mobility in soft soil is crucial to many military missions. Thus, it has been tested and quantified in a metric called Vehicle Cone Index (VCI) since World War II. VCI provides an index of the minimum soil strength necessary for vehicle mobility. The standard operating procedure for VCI field testing and data analysis is detailed herein. Also, a new method for quantifying VCI uncertainty has been proposed, which uses confidence bounds on mean measurements of soil strength. A sample analysis of actual field data is provided
Stevens, Maria T.Towne, Brent W.Osorio, Javier E.Mason, George L.
ABSTRACT Ground combat vehicles can operate in regions characterized by various types and severities of injuries – resulting from improvised explosive devices (IEDs), gunfire or heat illness – as well as extreme climates such as desert environments. Because of the wounded warrior’s compromised physical condition, their thermal surroundings within the vehicle are especially important. This paper presents insights gleaned from the Army medical community, as well as a simple study of the effect of heat on soldiers in a ground combat vehicle using CFD / thermal modeling and simulation tools and methodologies. In particular, an Army-patented method for controlling body temperature via skin temperature feedback together with a cooling vest and pants ensemble is employed
Tison, NathanSmith, Rob E.
ABSTRACT Motion planning algorithms for vehicles in an offroad environment have to contend with the significant vertical motion induced by the uneven terrain. Besides the obvious problems related to driver comfort, for autonomous vehicles, such “bumpy” vertical motion can induce significant mechanical noise in the real time data acquired from onboard sensors such as cameras to the point that perception becomes especially challenging. This paper advances a framework to address the problem of vertical motion in offroad autonomous motion control for vehicular systems. This framework is first developed to demonstrate the stabilization of the sprung mass in a modified quarter-car tracking a desired velocity while traversing a terrain with changing height. Even for an idealized model such as the quarter-car the dynamics turn out to be nonlinear and a model-based controller is not obvious. We therefore formulate this control problem as a Markov decision process and solve it using deep
Salvi, AmeyaBuzhardt, JakeTallapragada, PhanindraKrovi, VenkatBrudnak, MarkSmereka, Jonathon M.
This study aims to explore the multifaceted influencing factors of market acceptance and consumer behavior of low-altitude flight services through online surveys and advanced neuroscientific methods (such as functional magnetic resonance imaging fMRI, electroencephalography EEG, functional near-infrared spectroscopy fNIRS) combined with artificial intelligence and video advertisement quantitative analysis. We conducted an in-depth study of the current trends in low-altitude flight vehicle development and customer acceptance of low-altitude services, focusing particularly on the survey methods used for market acceptance. To overcome the influence of strong opinion leaders in volunteer group experiments, we designed specialized surveys targeting broader online and social media groups. Utilizing specialized knowledge in aviation psychology, we designed a distinctive questionnaire and, within just 7 days of its launch, gathered a significant number of valid responses. The data was then
Ma, XinDing, ShuitingLi, Yan
The life and safety of a battery are closely linked to temperature. Designing an effective thermal management system relies on a thorough understanding and analysis of the thermal properties and mechanisms of the battery. Over time, as batteries are used, their thermal characteristics change due to variations in internal SEI thickness, the deterioration of the active material structure, gas production, and electrolyte consumption, all of which are associated with the aging process. In this paper, experiments on both NCM and LFP batteries were made to measure the heat generation characteristics by adiabatic calorimeter. The results showed that the impact of calendar aging on battery heat generation exhibited completely different patterns for the lithium-ion batteries of the two material systems mentioned above. This paper provides guidance for the optimization of heat generation characteristics of battery and the calibration of heat source in the design of battery thermal management
Li, HaibinZhao, HongweiLiu, DinghongHu, Qiaosheng
With the capability of predicting detailed injury of occupants, the Human Body Model (HBM) was used to identify potential injuries for occupants in car impact events. However, there are few publications on using HBM in the aviation industry. This study aims to investigate and compare the head, neck, lumbar spine and thoracic responses of the Hybrid III and the THUMS (Total Human Model for Safety) model in the horizontal 26g and vertical 19g sled tests required by the General Aviation Aircraft Airworthiness Regulations. The HIC of THUMS and Hybrid III did not exceed the requirements of airworthiness regulations. Still, THUMS had higher intracranial pressures and intracranial stresses, which could result in brain injury to the occupants. In vertical impact, the highest stress of the neck of THUMS appears at the cervical spine C2 and the upper neck is easily injured; in horizontal impact, the cervical spine C7 has the highest load, and the lower neck is easily injured. Due to the low
Shi, XiaopengDing, XiangheGuo, KaiLiu, TianfuXie, Jiang
In non-cooperative environments, unmanned aerial vehicles (UAVs) have to land without artificial markers, which is a key step towards achieving full autonomy. However, the existing vision-based schemes have the common problems of poor robustness and generalization, and the LiDAR-based schemes have the disadvantages of low resolution, high power consumption and high weight. In this paper, we propose an UAV landing system equipped with a binocular camera to preform 3D reconstruction and select the safe landing zone. The whole system only consists of a stereo camera, and the innovation of the solution is fusing the stereo matching algorithm and monocular depth estimation(MDE) model to get a robust prediction on the metric depth. The whole landing system consists of a stereo matching module, a monocular depth estimation (MDE) module, a depth fusion module, and a safe landing zone selection module. The stereo matching module uses Semi-Global Matching (SGM) algorithm to calculate the
Zhou, YiBiaoZhang, BiHui
Integrating 3D point cloud and image fusion into flying car detection systems is essential for enhancing both safety and operational efficiency. Accurate environmental mapping and obstacle detection enable flying cars to optimize flight paths, mitigate collision risks, and perform effectively in diverse and challenging conditions. The AutoAlignV2 paradigm recently introduced a learnable schema that unifies these data formats for 3D object detection. However, the computational expense of the dynamic attention alignment mechanism poses a significant challenge. To address this, we propose a Lightweight Cross-modal Feature Dynamic Aggregation Module, which utilizes a model-driven feature alignment strategy. This module dynamically realigns heterogeneous features and selectively emphasizes salient aspects within both point cloud and image datasets, enhancing the differentiation between objects and the background and improving detection accuracy. Additionally, we introduce the Lightweight
Feng, XiaoyuZhang, RenhangChu, ZhengWei, LinaBian, ChenDuan, Linshuai
With the rapid advancement of Unmanned Aerial Vehicle (UAV) technology, their assigned missions have become significantly more intricate. Individual UAVs are no longer sufficient to meet these diverse and demanding requirements. There is now a shift towards employing multiple UAVs operating collaboratively to address complex tasks, replacing the reliance on singular units. This study focuses on the complexities of coordinated flight within UAV formations. A dynamic consensus optimal control algorithm is proposed for distributed formations, grounded in optimal control theory. Furthermore, the enhanced control method is validated via simulation on a semi-physical visualization platform, effectively closing the gap between real-world formation requirements and simulation outcomes. The results from these simulations underscore that the proposed method effectively preserves UAV formation integrity and demonstrates exceptional applicability in real-world scenarios
Li, WeiZhou, HanyunShi, JiekaiCheng, WeinanWang, FangBai, Jie
The fixed-wing VTOL is a new type of aircraft that combines the advantages of multi-rotor and fixed-wing aircraft. Enable freely taking off and landing, while maintaining high flight speeds during cruising. However, higher requirements for the powertrain system have emerged. The powertrain needs to adapt to the layout of distributed propulsion devices while also ensuring sufficient endurance. Both the full-electric powertrain and traditional fuel-based powertrain are unable to meet this demand, making the hybrid-electric powertrain one of the most feasible solutions currently available. A 10kW level hybrid-electric powertrain system was designed for a fixed-wing VTOL aircraft. The power generation performance tests are conducted to analyze the coupling working characteristics of the engine and generator. The performance of the hybrid configuration and the full-electric configuration in terms of power-to-weight ratio, energy-to-weight ratio, and endurance are compared. The results
Yanan, LiLi, HaiwangXie, GangSun, Mohan
An electric vertical take-off and landing aircraft (eVTOL) is a variety of vertical take-off aircraft driven by electric power. This work proposed a new boundary condition control method to investigate the take-off and landing process of eVTOL, which is under the conditions of a typical atmospheric boundary layer. The spatial flow field information, especially the height-dependent atmospheric crosswind velocity profile, will be projected on the temporal axis and superimposed with the existing time-dependent unsteady conditions. Taking a 4-axis eVTOL as an example, computational fluid dynamics (CFD) simulations based on unsteady Reynolds-Averaged Navier-Stokes (uRANS) and rigid body motion (RBM) are carried out with proposed unsteady boundary conditions. The loads and surrounding flow field of the aircraft are obtained, while the vortical structures are further identified and discussed. Notably, the impact of atmospheric boundary layer on the aerodynamic force of eVTOL during vertical
Wei, HuanxiaJia, ChundongShi, YongweiJia, QingXia, ChaoMo, RengYang, ZhigangLi, YanlongHu, Qiangqiang