Constrained spacecraft attitude control on SO(3) using fast nonlinear model predictive control-Reference-Cited by-同舟云学术

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Constrained spacecraft attitude control on SO(3) using fast nonlinear model predictive control

Published:2015-07 Issue: Volume: Page:
ISSN:
Container-title:2015 American Control Conference (ACC)
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Author:

Gupta Rohit,Kalabic Uros V.,Di Cairano Stefano,Bloch Anthony M.,Kolmanovsky Ilya V.

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx7/7160954/7170700/07171188.pdf?arnumber=7171188

Cited by 30 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

1. Model Predictive Control Based Reference Generation for Optimal Proportional Integral Derivative Control;2024 32nd Mediterranean Conference on Control and Automation (MED);2024-06-11

2. Autonomous Spacecraft Attitude Reorientation Using Robust Sampled-Data Control Barrier Functions;Journal of Guidance, Control, and Dynamics;2023-10

3. Adaptive Terminal Sliding Mode Fault-Tolerant Control of Spacecraft Based on the Left Attitude Error Function of SO(3);International Journal of Aerospace Engineering;2023-08-04

4. Deep Reinforcement Learning for Rendezvous and Attitude Control of CubeSat Class Satellite;2023 7th International Conference on Automation, Control and Robots (ICACR);2023-08-04

5. Neighboring extremal nonlinear model predictive control of a rigid body on SO(3);Robotica;2023-01-06

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