01588nas a2200157   4500008004100000245007200041210006900113260002900182520101900211653001301230100001901243700001101262700001601273700002001289856012101309       2006                        eng d00aAdaptive output feedback control of spacecraft relative translation0 aAdaptive output feedback control of spacecraft relative translat  aSan Diego, USAcDecember3 a<p>We address the problem of tracking relative translation in a leader-follower spacecraft formation using feedback from relative position only and under parameter uncertainty (spacecraft mass) and uncertainty in the leader variables (true anomaly rate and rate of change). We only assume boundedness of orbital perturbations and the leader control force but with unknown bounds. Under these conditions we propose a controller that renders the closed-loop system, uniformly semiglobally practically asymptotically stable. In particular, the domain of attraction can be made arbitrarily large by picking convenient gains, and the state errors in the closed-loop system are proved to converge from any initial condition within the domain of attraction to a ball in close vicinity of the origin in a stable way; moreover, this ball can be diminished arbitrarily by increasing the gains in the control law. Simulation results of a leader-follower spacecraft formation using the proposed controller are presented.</p>
10aRobotics1 aKristiansen, R1 aLor, A1 aChaillet, A1 aNicklasson, P J  uhttp://www.centropiaggio.unipi.it/publications/adaptive-output-feedback-control-spacecraft-relative-translation.html