Reliable strategies for implementing model-based navigation on fixed-wing drones

Gabriel Laupré, Lucas Pirlet, Jan Skaloud
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Abstract

A relatively novel approach of autonomous navigation employing platform dynamics as the primary process model raises new implementational challenges. These are related to: (i) potential numerical instabilities during longer flights; (ii) the quality of model self-calibration and its applicability to different flights; (iii) the establishment of a global estimation methodology when handling different initialisation flight phases; and (iv) the possibility of reducing computational load through model simplification. We propose a unified strategy for handling different flight phases with a combination of factorisation and a partial Schmidt–Kalman approach. We then investigate the stability of the in-air initialisation and the suitability of reusing pre-calibrated model parameters with their correlations. Without GNSS updates, we suggest setting a subset of the state vector as ‘considered’ states within the filter to remove their estimation from the remaining observations. We support all propositions with new empirical evidence: first in model-parameter self-calibration via optimal smoothing and second through applying our methods on three test flights with dissimilar durations and geometries. Our experiments demonstrate a significant improvement in autonomous navigation quality for twelve different scenarios.

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在固定翼无人机上实施基于模型导航的可靠策略
采用平台动力学作为主要过程模型的自主导航方法相对比较新颖,但也提出了新的实施挑战。这些挑战涉及(i) 长时间飞行中潜在的数值不稳定性;(ii) 模型自校准的质量及其对不同飞行的适用性;(iii) 在处理不同初始化飞行阶段时建立全局估算方法;以及 (iv) 通过简化模型减少计算负荷的可能性。我们结合因式分解和部分施密特-卡尔曼方法,提出了处理不同飞行阶段的统一策略。然后,我们研究了空中初始化的稳定性以及重新使用预校准模型参数及其相关性的适宜性。在没有全球导航卫星系统更新的情况下,我们建议将状态向量的一个子集设置为滤波器中的 "考虑 "状态,以便从剩余的观测数据中去除对这些状态的估计。我们用新的经验证据来支持所有主张:首先是通过优化平滑进行模型参数自校准,其次是将我们的方法应用于持续时间和几何形状各不相同的三次测试飞行。我们的实验证明,在十二种不同的情况下,自主导航的质量都有显著提高。
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