To enhance the accuracy of quadrotor UAV navigation systems in dynamic environments, we propose an attitude calculation method based on an acceleration correction model. This model estimates and corrects non-gravitational acceleration from the accelerometer, reducing its impact on attitude calculation. Experimental results demonstrate that this algorithm effectively mitigates non-gravitational acceleration interference and significantly improves the accuracy and anti-interference capability of UAV navigation systems.
No takes yet. Share an insight, caveat, or question.
Hongbo Fan (2024) studied this question.
Synapse has enriched 5 closely related papers on similar clinical questions. Consider them for comparative context: