Author:
Lincoln N. K.,Veres S. M.
Subject
Electrical and Electronic Engineering,Signal Processing,Control and Systems Engineering
Reference14 articles.
1. Analysis of Formation Flying Control of a Pair of Nanosatellites
2. . Global stabilisation of multibody spacecraft using quaternion-based nonlinear control law. Proceedings of the American Control Conference, Seattle, Washington, June 1995.
3. , . Output feedback control for spacecraft formation flying with coupled translation and attitude dynamics. Proceedings of the American Control Conference, Portland, OR, June 2005; 2419–2426.
4. Quaternion-Based Adaptive Attitude Tracking Controller Without Velocity Measurements
5. Universal adaptive control of satellite formation flying
Cited by
12 articles.
订阅此论文施引文献
订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献