A computational tool for conceptual design and optimization of planetary rovers

Q2 Engineering
A. Seeni, B. Schäfer
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引用次数: 0

Abstract

The design process of a Mars rover is driven by multiple design constraints, namely overall mass, power consumption and volume (dimensions). Various systems, such as mobility, manipulation, handling, power, thermal, communication, navigation, avionics and science instruments, together make a complete rover vehicle and they should function collectively to perform a given task. Each of the subsystems can be thought of as modular building blocks that are integrated together to form a fully functional rover vehicle. When approaching the design of such a vehicle, the designer should take into account of cross design dependencies existent between different subsystems and technology limitations. Performing any particular task, would lead to many design possibilities. Choosing the final design from many feasible solutions is arguably a daunting task. In order to make this process simple and convenient, as well as to understand the design non-linearity existing in this solution space, the authors have employed a systems engineering approach to develop a tool comprising subsystem models. The subsystem models comprise parametric and physics-based models. For designing suitable user-defined objectives, these models when integrated with Genetic Algorithm forms an effective tool to support design trade-offs during the conceptual design process. This integrated modeling and optimization approach is thought to be efficient in identifying rover system concepts.
行星漫游者概念设计与优化的计算工具
火星探测器的设计过程受到多重设计约束的驱动,即总体质量、功耗和体积(尺寸)。各种系统,如机动、操纵、搬运、动力、热、通信、导航、航空电子和科学仪器,共同构成了一个完整的漫游者车辆,它们应该共同发挥作用来执行给定的任务。每个子系统都可以被认为是模块化的构建块,它们集成在一起形成一个功能齐全的漫游车。在进行此类车辆的设计时,设计人员应考虑到不同子系统之间存在的交叉设计依赖关系和技术限制。执行任何特定的任务,都会导致许多设计可能性。从众多可行的解决方案中选择最终设计无疑是一项艰巨的任务。为了使这个过程简单和方便,以及理解存在于这个解空间中的设计非线性,作者采用了系统工程的方法来开发一个包含子系统模型的工具。子系统模型包括参数模型和基于物理的模型。为了设计合适的用户定义目标,这些模型与遗传算法相结合,形成了一个有效的工具,以支持在概念设计过程中的设计权衡。这种综合建模和优化方法被认为在识别漫游车系统概念方面是有效的。
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来源期刊
INCAS Bulletin
INCAS Bulletin Engineering-Aerospace Engineering
自引率
0.00%
发文量
50
审稿时长
8 weeks
期刊介绍: INCAS BULLETIN is a scientific quartely journal published by INCAS – National Institute for Aerospace Research “Elie Carafoli” (under the aegis of The Romanian Academy) Its current focus is the aerospace field, covering fluid mechanics, aerodynamics, flight theory, aeroelasticity, structures, applied control, mechatronics, experimental aerodynamics, computational methods. All submitted papers are peer-reviewed. The journal will publish reports and short research original papers of substance. Unique features distinguishing this journal: R & D reports in aerospace sciences in Romania The INCAS BULLETIN of the National Institute for Aerospace Research "Elie Carafoli" includes the following sections: 1) FULL PAPERS. -Strength of materials, elasticity, plasticity, aeroelasticity, static and dynamic analysis of structures, vibrations and impact. -Systems, mechatronics and control in aerospace. -Materials and tribology. -Kinematics and dynamics of mechanisms, friction, lubrication. -Measurement technique. -Aeroacoustics, ventilation, wind motors. -Management in Aerospace Activities. 2) TECHNICAL-SCIENTIFIC NOTES and REPORTS. Includes: case studies, technical-scientific notes and reports on published areas. 3) INCAS NEWS. Promote and emphasise INCAS technical base and achievements. 4) BOOK REVIEWS.
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