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Flight dynamics system design

机译:飞行动力系统设计

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Flight Dynamics Systems (FDS) are an integral component of every satellite ground system — they model and manage the orbital position and movement of satellites. As a global provider of satellite space and ground systems, Lockheed Martin has developed and deployed numerous FDSs for a wide-range of satellite systems. These in-house custom solutions were developed at a time when extensive analysis indicated that comparable commercial-off-the-shelf (COTS) capabilities did not exist in the market. Today, vendors are providing comparable, lower-cost, reliable, robust FDS capabilities. This project focuses on exploring the use of COTS products that can be more easily adapted to different satellites to reduce development time and life-cycle costs. The project evaluates how well each product satisfies Lockheed's needs, both in fulfilling technical requirements and in adaptability to Lockheed's existing systems. A comprehensive review of commercial off-the-shelf (COTS) flight dynamics systems identified three possible candidates as possible replacements for the current approach. These solutions, produced severally by Analytical Graphics Inc., A.I. Solutions, and GMV, were evaluated against a set of requirements and objectives developed in coordination with Lockheed Martin. Two systems, Satellite Toolkit (STK) from Analytical Graphics, and FreeFlyer from A.I. Solutions, were selected for prototype development in part due to their extensive number of prior installations and also limited access to GMV software. Prototype interfaces for STK and FreeFlyer were developed to simulate those systems' interactions with a notional satellite constellation and associated software suite, through several specific use cases. The goal of creating and testing the prototypes is to more deeply evaluate the challenges associated with customizing and adapting a COTS FDS through experiencing those challenges first-hand. Analysis revealed that STK's Java-based interfaces are more suite- to Lockheed's requirements, facilitating the required transfers natively. The socket-based connections available in FreeFlyer are sufficient for data exchange but increase processing overhead because of required intermediary steps.
机译:飞行动力学系统(FDS)是每种卫星地面系统的一体组件 - 它们的模型和管理卫星的轨道位置和运动。作为卫星空间和地面系统的全球提供商,洛克希德马丁已开发并为广泛的卫星系统开发并部署了许多FDS。这些内部定制解决方案是在广泛分析的广泛分析表明市场上不可应用的商业现货(COTS)能力不存在。今天,供应商提供可比,低成本,可靠,强大的FDS功能。该项目侧重于探索使用COTS产品,这些产品可以更容易地适应不同的卫星,以降低开发时间和生命周期成本。该项目评估了每个产品满足洛克希德的需求的需求,都在满足技术要求和对洛克希德现有系统的适应性方面。对商业现货(COTS)飞行动态系统的全面审查确定了三种可能的候选人,以适用于当前方法的替代品。这些解决方案是由分析图形Inc.的同期生产的,a.i。解决方案和GMV在与洛克希德马丁协调开发的一系列要求和目标中进行评估。来自分析图形的两个系统,卫星工具包(stk),以及a.i的Freeflyer。由于其广泛的现有安装以及对GMV软件的访问有限,因此选择了解决原型开发的原型开发。开发了STK和FreeFlyer的原型接口,以模拟这些系统与一个名义卫星星座和相关软件套件的交互,通过几种特定用例。创建和测试原型的目标是更深入地评估与定制和调整COTS FDS相关的挑战,通过体验挑战。分析表明,STK的基于Java的界面更套件到洛克希德的要求,促进了所需的转移。 FreeFlyer中可用的基于套接字的连接足以进行数据交换,但由于所需的中介步骤,增加处理开销。

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