Decentralized Estimation Algorithms for Formation Flying Spacecraft

نویسندگان

  • Philip Ferguson
  • Jonathan How
چکیده

Several space missions are being planned with large fleets of spacecraft at GEO and beyond where relative navigation using GPS will either be impossible or insufficient. Onboard local ranging devices will be required to replace or augment the available GPS measurements to perform relative navigation for these missions. The vast amounts of distributed data and the computational load limitations suggest that these navigation algorithms should be highly distributed, but the nonlinear local range measurements couple the states of the vehicles, which greatly complicates this decentralization. This paper investigates several estimator architectures and the associated algorithms for determining the fleet state, and then compares the resulting performance, computation, and communication requirements. This analysis shows that the proposed decentralized reducedorder filters provide near optimal estimation results without excessive communication or computation. Embedding these reduced-order estimators within the hierarchic architecture presented should permit scaling of the relative navigation to very large fleets.

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

Analysis of Decentralized Estimation Filters for Formation Flying Spacecraft

Future formation flying missions are being planned for fleets of spacecraft in MEO, GEO, and beyond where relative navigation using GPS will either be impossible or insufficient. To perform fleet estimation for these scenarios, local ranging devices on each vehicle are being considered to replace or augment the available GPS measurements. A previous paper presented several approaches for distri...

متن کامل

A Decentralized Scheme for Spacecraft Formation Flying via the Virtual Structure Approach

Built on the combined strength of decentralized control and the recently introduced virtual structure approach, a decentralized formation scheme for spacecraft formation flying is presented in this paper. Following a decentralized coordination architecture via the virtual structure approach, decentralized formation control strategies are introduced, which are appropriate when a large number of ...

متن کامل

Decentralized Scheme for Spacecraft Formation Flying via the Virtual Structure Approach

Built on the combined strength of decentralized control and the recently introduced virtual structure approach, a decentralized formation scheme for spacecraft formation flying is presented in this paper. Following a decentralized coordination architecture via the virtual structure approach, decentralized formation control strategies are introduced, which are appropriate when a large number of ...

متن کامل

Navigation Performance Predictions for the Orion Formation Flying Mission

This paper presents hardware-in-the-loop results that experimentally demonstrate precise relative navigation for true formation flying spacecraft applications. The approach is based on carrier-phase differential GPS, which is an ideal navigation sensor for these missions because it provides a direct measure of the relative positions and velocities of the vehicles in the fleet. In preparation fo...

متن کامل

Decentralized Relative Attitude Estimation for Three-Spacecraft Formation Flying Applications

This paper investigates the problem of relative spacecraft attitude estimation between three vehicles from a decentralized point of view. Decentralized attitude estimation is achieved through the use of local extended Kalman filters and a data fusion process known as the Covariance Intersection algorithm. Because the global attitude parameterization is the quaternion, the Covariance Intersectio...

متن کامل

Fault detection and isolation of the attitude control subsystem of spacecraft formation flying using extended Kalman filters

Abstract—In this paper, the problem of fault detection and isolation in the attitude control subsystem of spacecraft formation flying is considered. In order to design the fault detection method, an extended Kalman filter is utilized which is a nonlinear stochastic state estimation method. Three fault detection architectures, namely, centralized, decentralized, and semi-decentralized are design...

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 2003