2020 International Conference on Unmanned Aircraft Systems (ICUAS) 2020
DOI: 10.1109/icuas48674.2020.9213975
|View full text |Cite
|
Sign up to set email alerts
|

Aircraft Stall Recovery using Sliding-Mode Based Pitch-Attitude and Altitude Control

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
1

Citation Types

0
1
0

Year Published

2022
2022
2023
2023

Publication Types

Select...
4
1

Relationship

0
5

Authors

Journals

citations
Cited by 6 publications
(1 citation statement)
references
References 10 publications
0
1
0
Order By: Relevance
“…Furthermore, the history of SMC designed reveals that many aerospace control related problems have been solved apart from automatic landing. More explicitly, spiral, 20 stall, 21 spin entry, 22 spin recovery, 23,24 actuator fault 25,26 and reconfigurable flight control system designed 27 to name a few have been implemented using the SMC. Real-time applications in ref.…”
Section: Introductionmentioning
confidence: 99%
“…Furthermore, the history of SMC designed reveals that many aerospace control related problems have been solved apart from automatic landing. More explicitly, spiral, 20 stall, 21 spin entry, 22 spin recovery, 23,24 actuator fault 25,26 and reconfigurable flight control system designed 27 to name a few have been implemented using the SMC. Real-time applications in ref.…”
Section: Introductionmentioning
confidence: 99%