2012
DOI: 10.21236/ada572108
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On-board Model Predictive Control of a Quadrotor Helicopter: Design, Implementation, and Experiments

Abstract: Public reporting burden for the collection of information is estimated to average 1 hour per response, including the time for reviewing instructions, searching existing data sources, gathering and maintaining the data needed, and completing and reviewing the collection of information. Send comments regarding this burden estimate or any other aspect of this collection of information, including suggestions for reducing this burden, to Washington Headquarters Services, Directorate for Information Operations and R… Show more

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Cited by 54 publications
(47 citation statements)
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References 75 publications
(92 reference statements)
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“…Forces due to the atmosphere and gravitation act on the airframe in the global axes, these require that they be translated into the body from of axes before they can be introduced into the model: Using standard aerospace convention, the body frame rotation can be described in Earth coordinates in Euler angles (as shown in Figure 2). The rotational arguments can be combined to form the directional co-sine matrix DCM [3], [6], [7]:…”
Section: Rigid Body Analysis and Modellingmentioning
confidence: 99%
“…Forces due to the atmosphere and gravitation act on the airframe in the global axes, these require that they be translated into the body from of axes before they can be introduced into the model: Using standard aerospace convention, the body frame rotation can be described in Earth coordinates in Euler angles (as shown in Figure 2). The rotational arguments can be combined to form the directional co-sine matrix DCM [3], [6], [7]:…”
Section: Rigid Body Analysis and Modellingmentioning
confidence: 99%
“…An overview of the prediction parameters and their numerical values are given in Table 2. Values were chosen empirically and based on literature, such as [11,12] or examples from the ACADO toolkit.…”
Section: Nonlinear Model Predictive Control (Nmpc)mentioning
confidence: 99%
“…From several equations above, we have states of this quadcopter and its system output is [2] X = Al2xl2-£ + -012x4";/ = Ciaxl.…”
Section: A Linearized Quadcopter Modelmentioning
confidence: 99%