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Virtual prototype interface for the Air Force Manned SpacePlane project

机译：空军载人航天飞机项目的虚拟原型界面

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Abstract: The advent of requirements for worldwide deployment of space assets in support of Air Force operational missions has resulted in the need for a Manned SpacePlane (MSP) that can perform these missions with minimal preflight preparation and little, if any, in-orbit support from a mission control center. Because successful mission accomplishment will depend almost completely upon the MSP crew and the on-board capabilities of the spaceplane, the MSP user interface is a crucial component of successful mission accomplishment. In recognition of this fact, the USAF Phillips Laboratory in conjunction with USAF Space Command initiated the Virtual SpacePlane (VSP) project. To function effectively as an MSP interface development platform, the VSP must demonstrate the capability to simulate anticipated MSP missions and portray the MSP in operation throughout its entire flight regime, from takeoff through space operations and on to recovery via a horizontal landing at an airfield. Therefore, we architected, designed, and implemented a complete VSP that can be used to simulate anticipated Manned SpacePlane missions. The primary objective of the VSP is to be a virtual prototype for user interface design and development, the VSP software architecture and design facilities uncovering, refining and validating MSP user interface requirements. The Virtual SpacePlane reuses software components developed for the Virtual Cockpit and Solar System Modeler (SM) distributed virtual environment (DVE) applications, the Common Object Database (CODB) architecture, and Information Pod (Pod) interface tools developed in our labs. The Virtual Cockpit and Solar System Modeler supplied baseline interface components and tools, 3D graphical models, vehicle motion dynamics models, and DVE communication capabilities. Because we knew that the VSP's requirements would expand and evolve over the life of the project, we use the CODB architecture to facilitate our use of Rapid Evolutionary and Exploratory Prototyping to uncover application requirements and evaluate solutions. The Information Pod provides the paradigm and architectural framework for the user interface development. To achieve accurate and high fidelity performance for the VSP throughout its operational regime, the system integrates aerodynamics and astrodynamics models from the VC, SM and other sources into a single seamless high fidelity model of the VSP's dynamics. In this paper we discuss the background to the VSP project, its requirements, and the current user interface design. We summarize the VSP's current status and outline our plans for further VSP interface development and testing.!44
机译：摘要：为支持空军作战任务而在世界范围内部署空间资产的要求的出现，导致需要一种载人航天飞机（MSP），该飞机能够以最少的飞行前准备和很少（如果有的话）在轨支持来执行这些任务从任务控制中心由于成功完成任务几乎完全取决于MSP机组人员和太空飞机的机载能力，因此MSP用户界面是成功完成任务的关键组成部分。考虑到这一事实，美国空军菲利普斯实验室与美国空军太空司令部共同发起了虚拟太空飞机（VSP）项目。为了有效地充当MSP接口开发平台，VSP必须具备模拟预期的MSP任务并描绘MSP在其整个飞行状态下运行的能力，从起飞到太空运行一直到通过飞机场水平降落恢复为止。因此，我们设计，设计和实现了一个完整的VSP，可用于模拟预期的载人航天飞机任务。 VSP的主要目标是成为用于用户界面设计和开发，VSP软件体系结构和设计工具的虚拟原型，以发现，完善和验证MSP用户界面要求。 Virtual SpacePlane重用了为我们的实验室中开发的Virtual Cockpit和Solar System Modeler（SM）分布式虚拟环境（DVE）应用程序开发的软件组件，Common Object Database（CODB）体系结构以及Information Pod（Pod）接口工具。 Virtual Cockpit和Solar System Modeler提供了基准界面组件和工具，3D图形模型，车辆运动动力学模型以及DVE通信功能。因为我们知道VSP的需求会在项目的整个生命周期中扩展和发展，所以我们使用CODB架构来促进快速进化和探索性原型的使用，从而发现应用程序需求并评估解决方案。 Information Pod提供了用于用户界面开发的范例和体系结构框架。为了在整个运行过程中为VSP实现准确和高保真性能，该系统将来自VC，SM和其他来源的空气动力学和天体动力学模型集成到VSP动力学的单个无缝高保真模型中。在本文中，我们讨论了VSP项目的背景，其要求以及当前的用户界面设计。我们总结了VSP的当前状态，并概述了进一步VSP接口开发和测试的计划。！44

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