Browse Topic: Vehicle occupants
We present our ongoing efforts towards the development of crash-tolerant rotorcraft airframe structures through topology optimization, with the goal of enhancing energy absorption and occupant survival during vertical impact events. A high strain rate explicit dynamics solver has been developed, fully accelerated on GPUs, to enable rapid and accurate simulation of impact events critical to crashworthiness evaluation. In parallel, we have built a scalable three-dimensional topology optimization framework that enforces stiffness, weight, and frequency constraints simultaneously, driving structurally efficient and vibration-resistant designs. Benchmarking results demonstrate significant GPU-enabled speedups, facilitating high-fidelity crash simulations and large-scale optimization at practical turnaround times. This work establishes a computational foundation for future integration of crash-centric objectives and constraints into the optimization framework.
ABSTRACT Northrop Grumman has developed a software and hardware solution to provide enhanced 360 degree local situational awareness (LSA) to enable the warfighter with an overmatch capability on today’s modern battlefield. The architecture exploits technological gains in cameras, video processing, and video compression. The approach allows rapid comprehension of local and remote situational views presented with operational relevance for a ground combat platform or tactical wheeled platform crew. The 360 Degree LSA approach provides direct visualization of relative positioning of targets, threats, and lines of fire; and additionally offers common situational understanding / operational picture from the dismounted soldier to higher echelon commands. The approach provides prioritized information through LSA software to provide an enhanced view to the warfighter whereas the squad leader becomes an integral part of the crew with a view of the common operating picture (mounted) and additional sensors on tablet or handheld device (dismounted via wireless). The approach uses a platform agnostic form factor with components that can be selected and applied to legacy or new platforms based on their size, weight, power, and mission constraints.
Deos includes an industry standard lightweight TCP/IP stack (LwIP) with a DAL-A sockets library so it can provide data transport during in flight or on ground as part of its standard package. While it may have high data integrity (e.g., through CRC or other such mechanisms), TCP/IP over Ethernet is a non-deterministic protocol. As such, it is not suitable for avionics applications that require determinism or high robustness. In contrast, there are several are several redundant and deterministic data network technologies such as ARINC-664/AFDX, time triggered ethernet (TTE), and time sensitive networking (TSN). These interfaces are based on switched Ethernet technologies and can include system redundancy such that they are applicable for aircraft data network applications. Their feature set enables them to be used as a digital backbone for aircraft control and other applications where both integrity and availability are essential. Each of these solutions generally requires specific end point hardware to implement the protocols in firmware in order to meet the required communication timing and throughput. The implementation of the software device drivers for these technologies on Deos can leverage Deos' I/O Infrastructure (IOI) data distribution service for data decoupling. IOI is a DO-178 DAL-A module that can distribute data based on XML configuration files that specify the data paths, access control and optionally data formatting. It implements an inter-partition communications data interface between avionics applications including ARINC-653 partitions using the ARINC-653 APEX API sampling/queueing ports. Together, these features allow developers to readily adapt to changes in communication structures all through XML configuration files, versus recompiling which would impact the verification evidence of the module. This paper will talk about the different networking standards and how the use of Deos' IOI provides a way for the system to easily adapt to different network configurations without causing the driver library or end application(s) to be modified and thereby minimize change impact for reuse/reverification.
ABSTRACT
In this work, we present a lightweight pipeline for robust behavioral cloning of a human driver using end-to-end imitation learning. The proposed pipeline was employed to train and deploy three distinct driving behavior models onto a simulated vehicle. The training phase comprised of data collection, balancing, augmentation, preprocessing, and training a neural network, following which the trained model was deployed onto the ego vehicle to predict steering commands based on the feed from an onboard camera. A novel coupled control law was formulated to generate longitudinal control commands on the go based on the predicted steering angle and other parameters such as the actual speed of the ego vehicle and the prescribed constraints for speed and steering. We analyzed the computational efficiency of the pipeline and evaluated the robustness of the trained models through exhaustive experimentation during the deployment phase. We also compared our approach against state-of-the-art implementation in order to comment on its validity.
This SAE Information Report provides definitions and discussions of key terms concerning driver drowsiness and fatigue, and basic information on measuring drowsiness and fatigue. It also includes information and concepts for driver drowsiness as they relate to the safe operation of a vehicle. The key driver drowsiness and fatigue causal factors include the following: (1) sleep quality and quantity, (2) time of day, (3) time awake, (4) time on task (modulated by characteristics of the driving task), (5) task-related fatigue (variations of arousal levels related to task underload and overload), and (6) combinations of these factors. Medical conditions, medication, alcohol, or drugs exacerbate drowsiness; however, the discussion in this report is limited to fatigue concepts. This report has two primary outputs: (1) definitions and discussions of key terms concerning driver drowsiness and fatigue, and (2) basic information on measuring drowsiness and fatigue and its effects on the safe operation of a vehicle. These include the physiological and cognitive effects of driver drowsiness and fatigue on driving safety. Examples of effect of driver drowsiness and fatigue on driving safety include those related to vehicle control, operator vigilance (sustained attention), reaction times (object and event detection and response), situational awareness, physiological indicators, subjective assessments, and combinations thereof. For definitions of driving performance measures, refer to SAE J2944. This report applies to all worldwide motor vehicle passenger cars and light trucks, as well as heavy trucks, buses, motorcycles, and mopeds. The intended users of the document are practitioners and researchers in the automotive industry, academia, and other organizations with interest in driver drowsiness and fatigue, driving and driver performance assessment, and road safety.
This research sought to distill and define the fundamentals of system and software architecture analysis and form the basis by which a design can be tested and analyzed prior to its implementation. In short, the question "can a design be measured against the business-level objectives and quality-of-use architectural requirements. The research focuses on building a body of knowledge that supports an analysis, built on fundamentals which scales and can serve as the basis by which we can transform when and how architecture validation can occur. This research supports ongoing work towards developing a strategic comprehensive architecture approach and extends the analysis and documentation of the Key Business Drivers (KBDs) and architectural drivers supporting the efficient development and sustainment of interoperable aviation mission systems. A prototype process that leverages the discovered relationships and weights for use by current Architects and Senior Systems Engineers is shown. Programs implementing this approach are expected to benefit from the planned reuse of architectural artifacts for follow up systems engineering products supporting the development of reusable component product lines avoiding the long-term challenges of unrealized architectural objectives.
The serial introduction of passive and active anti-vibration means lead primarily to the reduction of the vibration levels at blade passage frequencies Nb/rev. Consequently, other- previously unnoticed- sources of vibration are perceived by rotorcraft occupants. Therefore, a comprehensive vibration assessment metric is required to characterize the impact of different vibration sources of helicopters regarding passenger comfort. Since the advance of industrial/military aerial transport machines, several vibration assessment metrics were developed such as the Intrusion Index (ADS-27A-SP), the overall ride value av (ISO2631-1) and the NASA DISC model. However, these metrics have deficiencies regarding the evaluation of complex rotorcraft vibrations, e.g. the Intrusion Index favors only the rotor harmonics in the vibration evaluation, the overall ride value av is based on uniaxial, sinusoidal oscillations at discrete frequencies and the NASA DISC model considers only vibration measurements on the floor and not on other vibration contact surfaces. Since the rotorcraft vibrations are characterized by the presence of triaxial, multiple vibration sources it is unclear whether one of these metrics is appropriate to assess the perceived discomfort. The work presented in this paper addresses this topic. The suitability of existing vibration evaluation metrics, especially av, regarding typical rotorcraft vibration patterns is investigated. For that purpose, a systematic whole-body vibration campaign was performed, in which human subjects were seated in a helicopter seat on a motion platform and exposed to helicopter specific vibration patterns of which specific frequencies were systematically attenuated or increased. Participants rated the perceived discomfort using magnitude estimation. The campaign reveals, that the overall ride value av is not well-suited to predict and to compare the discomfort of different vibration spectra. Especially in vertical direction, the application of av will significantly overestimate the discomfort. This implies that this metric is not appropriate for evaluation of helicopter specific vibrations and could be improved. The results in this paper are a first step in that direction but more comprehensive analyses of helicopter specific vibrations and their impact on passenger comfort are necessary.
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