2020
DOI: 10.1007/s42405-020-00273-8
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Flight Control Design using Incremental Nonlinear Dynamic Inversion with Fixed-lag Smoothing Estimation

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Cited by 7 publications
(4 citation statements)
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“…e so-called model identification refers to the estimation and judgment of parameters such as coefficients and lag period in the model [22][23][24].…”
Section: Pvar Model Identificationmentioning
confidence: 99%
“…e so-called model identification refers to the estimation and judgment of parameters such as coefficients and lag period in the model [22][23][24].…”
Section: Pvar Model Identificationmentioning
confidence: 99%
“…By producing the incremental form of the control command by calculating the error between the virtual control law and the acceleration of the system state, INDI is robust to model uncertainties [12][13][14][15][16][17][18][19]. In [17], the stability and robustness of the INDI technique has been proven.…”
Section: Introductionmentioning
confidence: 99%
“…The policy evaluation step is outlined in Eq. (1), where ( , | , ) defines the probability of a subsequent state, , occurring with the respective reward, . Furthermore, ( | ) denotes the probability of an action to be taken at a given state, .…”
Section: Introductionmentioning
confidence: 99%
“…Consequently, controllers that can be derived using data-driven methods are preferred in such cases. Advanced sensor-based controllers exist, such as incremental dynamic inversion controllers [1], to alleviate the burden of modelling complex systems. However, the aforementioned methods suffer from state reconstruction dependencies and synchronisation issues with the sensor data.…”
mentioning
confidence: 99%