Hardware-in-the-Loop Simulation of an Extended Non-Linear Dynamic Inversion Augmented with an Immunity-Based Adaptive Control System-Reference-Cited by-同舟云学术

Hardware-in-the-Loop Simulation of an Extended Non-Linear Dynamic Inversion Augmented with an Immunity-Based Adaptive Control System

Published:2013-08-15 Issue: Volume: Page:
ISSN:
Container-title:AIAA Modeling and Simulation Technologies (MST) Conference
language:
Short-container-title:

Author:

Lyons Brendon¹,Moncayo Hever¹,Noriega Alfonso¹,Moguel Israel¹,Perhinschi Mario G.²

Affiliation:

1. Embry-Riddle Aeronautical University

2. West Virginia University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2013-5152

Reference24 articles.

1. 5Ito D., Georgie J., Valasek J., Ward D., Re-Entry Vehicle Flight Controls Design Guidelines: Dynamic Inversion, Final Technical Report , NAG9-1085, Flight SimulationLaboratory, Texas Engineering Experiment Station, Texas A&MUniversity. 23May2000"-23 May2001.

Cited by 5 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. Comparison of Optimal and Bioinspired Adaptive Control Laws for Spacecraft Sloshing Dynamics;Journal of Spacecraft and Rockets;2020-01

2. Spacecraft Heath Monitoring Using a Biomimetic Fault Diagnosis Scheme;Journal of Aerospace Information Systems;2018-07

3. Spacecraft Health Monitoring Using a Biomimetic Fault Diagnosis Scheme;AIAA Information Systems-AIAA Infotech @ Aerospace;2017-01-05

4. Control Laws Development for a Free-Flying Unmanned Robotic System to Support Interplanetary Bodies Prospecting and Characterization Missions;AIAA Guidance, Navigation, and Control Conference;2016-01-01

5. A Bio-Inspired Adaptive Control Compensation System for an Aircraft Outside Bounds of Nominal Design;Journal of Dynamic Systems, Measurement, and Control;2015-09-01