Decomposition and Control of Multiple Spacecraft Formation Flying

نویسندگان

  • Dongjun Lee
  • Perry Y. Li
چکیده

We propose a novel control framework for the formation flying of multiple spacecraft. With the passive decomposition, group dynamics of the multiple spacecraft is decomposed into two decoupled dynamics: the shape system representing the internal group formation shape (formation, in short), and the locked system describing the total group maneuver (maneuver, in short). Then, some desired formation and maneuver of the group can be simultaneously achieved by controlling the shape and locked systems individually. Also, due to the decoupling between the shape and locked systems, high precision maneuver and tight formation can be achieved without any dynamic crosstalk between them. By connecting all group agents via bi-directional controls so that slower agents are prevented from being left behind, the proposed scheme enforces a coherence among the agents as one group. Abstracting a group by its locked system whose dynamics is similar to that of a single spacecraft, the proposed control scheme can also impose an hierarchy for a mixed collection of many agents and groups. We also provide a decentralization of the proposed control scheme for applications where only neighboring sensings (or communications) are available. Simulations are performed to illustrate properties of the proposed control schemes.

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

Fuzzy Sliding Mode for Spacecraft Formation Control in Eccentric Orbits

The problem of relative motion control for spacecraft formation flying in eccentric orbits is considered in this paper. Due to the presence of nonlinear dynamics and external disturbances, a robust fuzzy sliding mode controller is developed. The slopes of sliding surfaces of the conventional sliding mode controller are tuned according to error states using a fuzzy logic and reach the pre-define...

متن کامل

A Survey of Spacecraft Formation Flying Guidance and Control (Part 11): Control

Abstruct-Formation flying is defined as a set of more than one spacecraft whose states are coupled through a common control law. This paper provides a comprehensive survey of spacecraft formation flying control (FFC), which encompasses design techniques and stability results for these coupled-state control laws. We divide the FFC literature into five FFC architectures: (i) Multiple-Input Multip...

متن کامل

High Accuracy Relative Motion of Spacecraft Using Linearized Time-Varying J2-Perturbed Terms

This paper presents a set of linearized equations was derived for the motion, relative to an elliptical reference orbit, of an object influenced by J2 perturbation terms. Approximate solution for simulations was used to compare these equations and the linearized keplerian equations to the exact equations. The inclusion of the linearized perturbations in the derived equations increased the high ...

متن کامل

Aas 00-109 Precise Formation Flying Control of Multiple Spacecraft Using Carrier-phase Differential Gps1

Formation flying is a key technology for deep space and orbital applications that involve multiple spacecraft operations. Imaging and remote sensing systems based on radio interferometry and SAR require very precise (subwavelength) aperture knowledge and control for accurate relative data collection and processing. Closely tied with the Orion and TechSat21 projects, this work describes the ongo...

متن کامل

Spacecraft formation stabilization and fault tolerance: A state-varying switched system approach

The focus of this paper is the spacecraft formation flying problem where the formation switches successively among multiple shapes, the number and the composition of spacecraft in the group may change among these shapes, and some spacecraft may be faulty. The whole flying process is modeled as a state-varying switched system. The formation stability and fault tolerability are analyzed by using ...

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 2004