2022
DOI: 10.1109/taes.2021.3123215
|View full text |Cite
|
Sign up to set email alerts
|

Increased Robustness to Delay in Incremental Controllers Using Input Scaling Gain

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
3
1
1

Citation Types

0
13
0

Year Published

2022
2022
2023
2023

Publication Types

Select...
4
1
1

Relationship

0
6

Authors

Journals

citations
Cited by 13 publications
(13 citation statements)
references
References 22 publications
0
13
0
Order By: Relevance
“…It is assumed that the higher order terms can be neglected. The control law is obtained by solving (19) for 𝑢 𝑐 :…”
Section: Comparison With Incremental Nonlinear Dynamic Inversionmentioning
confidence: 99%
See 3 more Smart Citations
“…It is assumed that the higher order terms can be neglected. The control law is obtained by solving (19) for 𝑢 𝑐 :…”
Section: Comparison With Incremental Nonlinear Dynamic Inversionmentioning
confidence: 99%
“…It can further be shown, that the input scaling as suggested by Cordeiro et al [18] and [19] for reducing the influence of noise and increasing the robustness with respect to time delays, can be interpreted as a modification of the innermost bandwidth of 𝑦: Ω 𝑦 = Λ𝜔, where the input scaling gain matrix Λ ∈ R 𝑚×𝑚 is diagonal. If this relation is inserted into (16), and it is assumed that the actuators have equal bandwidth, i.e.…”
Section: Comparison With Incremental Nonlinear Dynamic Inversionmentioning
confidence: 99%
See 2 more Smart Citations
“…To guarantee the precision of the aerial imagery coverage, the mission definition of the flying wing UAV after remote cut-off from the HAB, and respective trajectory control, is essential. The implementation of nonlinear control solutions robust to wind disturbances and model uncertainties take gain from its gliding flight capabilities, guaranteeing the mission execution while maximizing flight time (Cordeiro et al (2021)). An example of a UAV mission after deployment from HAB and stabilization, and simulated execution, is presented in Figure 3, where several points of interest are surveyed (vertical range was greatly reduced to limit the resulting loitering turns on descent).…”
Section: High-altitude Balloon In Fire-fighting Operationsmentioning
confidence: 99%