AstroSat is India’s first dedicated astronomical observatory in space with multi-wavelength payload on a single platform. It enables simultaneous observations in the desired wavebands. The increase in the number of payloads has also led to an increase in the complexity in space segment design, ground segment design, and mission operation management. Each payload instrument and mainframe has its own constraint for the operation, which needs to be satisfied to ensure the safety of the systems. In this paper, we explain the challenges in ground operations for mission management with various constraints. Also, we list the various constraints, both geometric and otherwise, with respect to the mainframe systems and payload instruments of AstroSat.

AstroSat 是印度第一个在单一平台上具有多波长有效载荷的太空专用天文台。它可以在所需波段中同时进行观测。有效载荷数量的增加也导致空间段设计、地面段设计和任务运行管理的复杂性增加。每个有效载荷仪器和主机都有自己的操作约束，需要满足这些约束以确保系统的安全。在本文中，我们解释了具有各种约束条件的任务管理的地面操作挑战。此外，我们列出了与 AstroSat 的大型机系统和有效载荷仪器有关的各种约束，包括几何约束和其他约束。