Parameter Governors for Coordinated Control of n-Spacecraft Formations

نویسندگان
چکیده

برای دانلود باید عضویت طلایی داشته باشید

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

اگر عضو سایت هستید لطفا وارد حساب کاربری خود شوید

منابع مشابه

Dynamic Synchronization of Spacecraft Modeling and Coordinated Control of Leader-Follower Spacecraft Formations

The work reported in this thesis proposes several solutions to coordination control of relative motion between spacecraft in a leader-follower formation. In this framework , detailed models of spacecraft relative translation and relative rotation in elliptical Earth orbits are derived, based on the principles of Newtonian mechanics and Euler's moment equation, and subsequently collected in one ...

متن کامل

Coordinated Attitude Control of Flexible Spacecraft Formations via Behavior-based Control Approach

This paper is to investigate the coordinated attitude control problem for flexible spacecraft formations. Considering the attitude maneuver control problem of a formation composed of flexible spacecraft, two classes of decentralized attitude coordination control laws using behavior-based control approach are proposed. The first class of controllers can steer the attitude states of the flexible ...

متن کامل

Robust Load-sharing Control of Spacecraft Formations

This paper focuses on the design of autonomous and collaborative control strategies to govern the relative distances among multiple spacecraft in formation with no ground intervention. A coordinate load-sharing control structure for formation flying and a methodology to control their dynamic models with slow t ime-varymg and uncertain parameters are the main objectives of this work. The method ...

متن کامل

Optimal Continuous/Impulsive Control for Lorentz-Augmented Spacecraft Formations

a = semimajor axis b = magnetic field vector e = eccentricity e = orbital element vector e · = matrix exponential f = true anomaly h = angular momentum magnitude i = inclination J = cost Jn = nth zonal harmonic coefficient M = mean anomaly m = mass m = magnetic dipole vector N − 1 = number of thrusts n = mean motion p = semilatus rectum q = electrical charge r = orbit radius magnitude r = posit...

متن کامل

Attitude Control of Spacecraft Formations Subject To Distributed Communication Delays

This paper considers the problem of achieving attitude consensus in spacecraft formations with bounded, time-varying communication delays between spacecraft connected as specified by a strongly connected topology. A state feedback controller is proposed and investigated using a time domain approach (via LMIs) and a frequency domain approach (via the small-gain theorem) to obtain delay dependent...

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

ژورنال

عنوان ژورنال: Journal of Guidance, Control, and Dynamics

سال: 2017

ISSN: 0731-5090,1533-3884

DOI: 10.2514/1.g002539