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Kasey Ackerman
Kasey Ackerman
NASA Langley Research Center
在 nasa.gov 的电子邮件经过验证
标题
引用次数
引用次数
年份
-Adaptive MPPI Architecture for Robust and Agile Control of Multirotors
J Pravitra, KA Ackerman, C Cao, N Hovakimyan, EA Theodorou
2020 IEEE/RSJ International Conference on Intelligent Robots and Systems …, 2020
732020
Evaluation of an Adaptive Flight Control Law on Calspan’s Variable-Stability Learjet
KA Ackerman, E Xargay, R Choe, N Hovakimyan, MC Cotting, RB Jeffrey, ...
Journal of Guidance, Control, and Dynamics, 2017
482017
stability augmentation system for Calspan’s variable-stability Learjet
KA Ackerman, E Xargay, R Choe, N Hovakimyan, MC Cotting, RB Jeffrey, ...
AIAA Guidance, Navigation, and Control Conference, 2016-0631, 2016
44*2016
Tube-certified trajectory tracking for nonlinear systems with robust control contraction metrics
P Zhao, A Lakshmanan, K Ackerman, A Gahlawat, M Pavone, ...
arXiv preprint arXiv:2109.04453, 2021
402021
Automation Situation Awareness Display for a Flight Envelope Protection System
KA Ackerman, DA Talleur, RS Carbonari, E Xargay, BD Seefeldt, A Kirlik, ...
Journal of Guidance, Control, and Dynamics, 2017
382017
Adaptive Augmentation for Geometric Tracking Control of Quadrotors
Z Wu, S Cheng, KA Ackerman, A Gahlawat, A Lakshmanan, P Zhao, ...
2022 International Conference on Robotics and Automation (ICRA), 1329-1336, 2022
342022
Controller Design for Propeller Phase Synchronization with Aeroacoustic Performance Metrics
A Patterson, NH Schiller, KA Ackerman, A Gahlawat, IM Gregory, ...
AIAA Scitech 2020 Forum, 1494, 2020
252020
Recovery of Desired Flying Characteristics with an Adaptive Control Law: Flight Test Results on Calspan's VSS Learjet
K Ackerman, J Puig-Navarro, N Hovakimyan, MC Cotting, DJ Duke, ...
AIAA Scitech 2019 Forum, 1084, 2019
222019
Flight envelope information-augmented display for enhanced pilot situation awareness
KA Ackerman, BD Seefeldt, E Xargay, DA Talleur, RS Carbonari, A Kirlik, ...
AIAA Guidance, Navigation, and Control Conference, 2015-1112, 2015
212015
Trajectory Generation for Noise-Constrained Autonomous Flight Operations
KA Ackerman, IM Gregory
AIAA Scitech 2020 Forum, 0978, 2020
152020
An Adaptive Stability Augmentation System Designed for MIL-HDBK-1797 Level 1 Flying Qualities
J Puig-Navarro, K Ackerman, N Hovakimyan, MC Cotting, DJ Duke, ...
AIAA Scitech 2019 Forum, 1083, 2019
152019
‘Can I Get On?!’ Providing Consistent Handling Qualities on Calspan’s Variable-Stability Learjet
MC Cotting, RB Jeffrey, MP Blackstun, TP Fulkerson, TR Lau, ...
AIAA Guidance, Navigation, and Control Conference, 2016-0632, 2016
15*2016
Quad: Adaptive Augmentation of Geometric Control for Agile Quadrotors with Performance Guarantees
Z Wu, S Cheng, P Zhao, A Gahlawat, KA Ackerman, A Lakshmanan, ...
arXiv preprint arXiv:2302.07208, 2023
132023
Flight Control Methods for Multirotor UAS
KA Ackerman, IM Gregory, N Hovakimyan
International Conference on Unmanned Aircraft Systems, 2019
122019
Evolving Relationship between Humans and Machines
AC Trujillo, IM Gregory, KA Ackerman
2nd IFAC Conference on Cyber-Physical & Human Systems, 2018
122018
Pilot-in-the-loop flight simulator for NASA’s Transport Class Model
KA Ackerman, ST Pelech, RS Carbonari, N Hovakimyan, A Kirlik, ...
AIAA Guidance, Navigation, and Control Conference, 2014-0613, 2014
122014
Trajectory Generation for Distributed Electric Propulsion Vehicles with Propeller Synchronization
A Patterson, KA Ackerman, N Hovakimyan, IM Gregory
AIAA Scitech 2021 Forum, 0586, 2021
82021
Autonomous Path-Following for a Tilt-Wing, Distributed Electric Propulsion, Vertical Take-Off and Landing Unmanned Aerial System in Hover Mode
JR Cooper, KA Ackerman, PM Rothhaar, IM Gregory
82018
Feedback Control of Flight Speed to Reduce Unmanned Aerial System Noise
MB Galles, NH Schiller, KA Ackerman, BA Newman
2018 AIAA/CEAS Aeroacoustics Conference, 2950, 2018
72018
Design and Evaluation of an Adaptive Controller for NASA’s Transport Class Model
J Dodenhöft, R Choe, K Ackerman, F Holzapfel, N Hovakimyan
AIAA Guidance, Navigation, and Control Conference, 1250, 2017
62017
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