Aas 03-125 Historical Review of Spacecraft Simulators
نویسندگان
چکیده
This paper provides an overview of air-bearing spacecraft simulators. Air bearings have been used for satellite attitude determination and control hardware verification and software development for nearly 45 years. Honeywell Space Systems and Virginia Tech are each developing unique new facilities. During their development, we have become interested in the history of this technology: how early systems were first devised, and what diverse capabilities current systems provide. We begin with a survey of planar systems, those that give a payload freedom to translate and spin. We then discuss several classes of rotational air bearings which simulate three-axis satellite attitude dynamics. We follow with a section on perhaps the most interesting facilities: those that provide both translational and three-parameter rotational freedom. We outline the diverse capabilities each style of air-bearing testbed provides, the many settings they can be found in, and ways to improve facility performance.
منابع مشابه
Aas 03-611 Comparison of System Identification Techniques for a Spherical Air-bearing Spacecraft Simulator
Virginia Tech has developed a testbed comprised of two independent spherical air-bearing platforms for formation flying attitude control simulation, the Distributed Spacecraft Attitude Control System Simulator. The DSACSS is intended to support a wide range of functions; as such, requiring that all controllers be robust to approximations of the system parameters is impractical. We document the ...
متن کاملHistorical Review of Air-Bearing Spacecraft Simulators
An overview of air-bearing spacecraft simulators is provided. Air bearings have been used for satellite attitude determination and control hardware veri cation and software development for nearly 45 years. It is interesting to consider the history of this technology: how early systems were rst devised and what diverse capabilities current systems provide. First a survey is given of planar sy...
متن کاملRobust Attitude Control of Spacecraft Simulator with External Disturbances
The spacecraft simulator robust control through H∞-based linear matrix inequality (LMI) and robust adaptive method is implemented. The spacecraft attitude control subsystem simulator consists of a platform, an air-bearing and a set of four reaction wheels. This set up provides a free real-time three degree of freedom rotation. Spacecraft simulators are applied in upgrading and checking the c...
متن کاملAas 03-103 Structured Model Reference Adaptive Control for Vision Based Spacecraft Rendezvous and Docking
A structured model reference adaptive control law has been developed for vision based spacecraft rendezvous and docking problem. A highly accurate relative motion of chaser spacecraft can be estimated by processing the reliable high bandwidth measurements of newly developed VISNAV sensor through a nonlinear geometric estimation process. The adaptive control law formulation is based upon the Lya...
متن کاملAas 04-122 System Identification of a Spherical Air-bearing Spacecraft Simulator
The Distributed Spacecraft Attitude Control System Simulator is a testbed comprised of two independent spherical air-bearing platforms, useful for formation-flying attitude control simulation. The DSACSS is intended to support a wide range of functions. As such, requiring that all controllers be robust to approximations of the system parameters is impractical. We document the development of bat...
متن کاملذخیره 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 2003