Satellite Cluster Command and Control

نویسنده

  • Paul Zetocha
چکیده

For many applications a distributed cluster of cooperating satellites offers distinct advantages over satellites functioning alone. These include optimization of mission performance and increased fault tolerance. Although there are many benefits, commanding and controlling a large cluster of cooperating satellites poses several challenges. These include how satellites in the cluster maintain knowledge of the other satellites in the cluster in order to react to contingencies and optimize resources, how to treat the cluster as a single virtual satellite in terms of ground command and control, and how to distribute resources across the cluster. The Space Vehicles Directorate of the Air Force Research Laboratory (AFRL) is investigating many of these challenges through prototype development for the AFRL TechSat-21 program. This paper presents the challenges posed in cluster command and control and discusses several methods being developed to address those challenges.

برای دانلود رایگان متن کامل این مقاله و بیش از 32 میلیون مقاله دیگر ابتدا ثبت نام کنید

ثبت نام

اگر عضو سایت هستید لطفا وارد حساب کاربری خود شوید

منابع مشابه

An efficient method to control the amplitude of the limit cycle in satellite attitude control system

In this paper, an efficient method is presented to control the attitude of a satellite with ON-OFF actuator. The main objective of this novel method is to control the amplitude of the limit cycle which commonly appears in the steady state of such systems; and at the same time by consideration of real actuator constraints, reduce the fuel consumption of system. The Proposed method is a combinati...

متن کامل

A Distributed Flight Software Design for Satellite Formation Flying Control

Several NASA and DoD missions are envisioned that will utilize distributed, autonomous clusters of spacecraft. The Air Force Research Laboratory initiated the TechSat 21 mission to demonstrate the key enabling technologies of formation flying and distributed radar. Princeton Satellite Systems developed the Formation Flying Module (FFM) for TechSat 21 to provide autonomous reconfiguration, forma...

متن کامل

Command and Control of a Cluster of Satellites

There is an increasing desire in many organizations, including NASA and the DoD, to use constellations or fleets of autonomous spacecraft working together to accomplish complex mission objectives. At the Air Force Research Laboratory’s (AFRL) Space Vehicles Directorate we are investigating and developing architectures for commanding and controlling a cluster of cooperating satellites. For many ...

متن کامل

Near-Minimum Time Optimal Control of Flexible Spacecraft during Slewing Maneuver

The rapid growth of space utilization requires extensive construction, and maintenance of space structures and satellites in orbit. &#10This will, in turn, substantiate application of robotic systems in space. In this paper, a near-minimum-time optimal control law is developed for a rigid space platform with flexible links during an orientating maneuver with large angle of rotation. The time op...

متن کامل

COMPARISON BETWEEN MINIMUM AND NEAR MINIMUM TIME OPTIMAL CONTROL OF A FLEXIBLE SLEWING SPACECRAFT

In this paper, a minimum and near-minimum time optimal control laws are developed and compared for a rigid space platform with flexible links during an orientating maneuver with large angle of rotation. The control commands are considered as typical bang-bang with multiple symmetrical switches, the time optimal control solution for the rigid-body mode is obtained as a bang-bang function and app...

متن کامل

ذخیره در منابع من


  با ذخیره ی این منبع در منابع من، دسترسی به آن را برای استفاده های بعدی آسان تر کنید

عنوان ژورنال:

دوره   شماره 

صفحات  -

تاریخ انتشار 2000