2014
DOI: 10.1002/navi.68
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Model-Aided Navigation for a Quadrotor Helicopter: A Novel Navigation System and First Experimental Results

Abstract: This paper presents a novel navigation system for aiding a classic inertial navigation system with a Vehicle Dynamics Model in a quadrotor application. The navigation system is based on the previously presented Unified Model technique for optimal fusion of the two prediction models. The key point of the approach in this paper is that the required modeling and implementation effort is minimized by incorporating a translational dynamics model only. Even though no rotational vehicle dynamics are modeled, it is sh… Show more

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Cited by 29 publications
(26 citation statements)
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“…Among the suggested methods, the integrated system of model‐aided navigation introduced in reduces the computational complexity and cost, while it is mathematically equivalent to the parallel implementation and virtual observation system. This system is also successful in experimental and laboratory tests …”
Section: Introductionmentioning
confidence: 88%
“…Among the suggested methods, the integrated system of model‐aided navigation introduced in reduces the computational complexity and cost, while it is mathematically equivalent to the parallel implementation and virtual observation system. This system is also successful in experimental and laboratory tests …”
Section: Introductionmentioning
confidence: 88%
“…Based on their previous work regarding the unified KF model, and in order to minimize the effort required in the modeling of the Quadcopter UAV parameters, in , instead of employing the rotational and the translational VDM, they use the translation VDM only, because according to their approach, it requires a lot of effort in parametrization and identification of the UAV model. During simulation, they assumed no wind and also a perfect DM, just so that they could verify the enhancement capability in using the translation VDM to aid the INS.…”
Section: Related Workmentioning
confidence: 99%
“…Therefore, IMU failure disables navigation in this case as well. In many cases, the presence of wind is not considered , or the capability of correcting the parametric errors in the dynamic model on‐flight is not provided , or the VDM is included only partially within the filter . Some researchers also consider IMUs of higher accuracy , which is impractical for small UAVs in terms of size/weight and cost.…”
Section: Introductionmentioning
confidence: 99%
“…In a recent study, Crocoll et al . proposed and tested a navigation system for a quadcopter UAV that was aided by a translational dynamics model. The authors unified the VDM and INS before the Kalman filter prediction step to reduce computation cost and improve stability.…”
Section: Introductionmentioning
confidence: 99%
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