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Multi-Source Interactive Resilient Fusion Algorithm Based on RIEKF

Signal Processing · Submitted 2 Mar 2024

abstract compiled · 2026-09-23 · no language-model review

The authors' main claim Experimental results show that the algorithm presented in this paper, without using any sensor fault diagnosis and isolation logic, without setting any complex detection timing and thresholds, demonstrates a resilience advantage, thereby enhancing the adaptability of the state estimation system in complex environments.

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arXiv ID2403.01134 (version 1)
Pith IDBOK5FA6X, Pith's permanent record of this paper and its review
CitationSong Fujun, Ye Xiaoyu, Zeng Qinghua, Zhu Xiaohu. "Multi-Source Interactive Resilient Fusion Algorithm Based on RIEKF." arXiv:2403.01134 (2024). https://pith.science/paper/BOK5FA6X
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What the abstract itself states, as probabilities: claims first 0.04 · states limitation 0.19 · human participants 0.02 · controlled comparison 0.09 · randomized assignment 0.01 · states quantitative result 0.04 · compares with prior results 0.12 · mentions code or data availability 0.02.

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arXiv listing abstract v1. Results and the main claim are underlined; .

As the number of heterogeneous redundant sensors on unmanned aerial vehicle (UAV) increases, onboard sensors require a more rational and efficient credibility evaluation system and a resilient fusion framework to achieve the essence of seamless sensor group switching. A simple and efficient sensor credibility evaluation system is proposed to guide the selection of the optimal multi-source sensor submodel combination, thereby providing key model prior knowledge for multi-source resilient fusion. Furthermore, a multi-model interactive resilient fusion framework based on RIEKF is proposed, utilizing the defined sensor credibility indexes to guide the design of the model transition probability matrix, thereby reducing the sensitivity of submodel weights to fusion stability and solving the problem of the model transition matrix lacking a basis for adjustment. Model weights are updated in real time through credibility prior information and submodel posterior probabilities, thus leveraging the adaptive resilience advantage between models to achieve seamless switching between submodels in complex environments. Experimental results show that the algorithm presented in this paper, without using any sensor fault diagnosis and isolation logic, without setting any complex detection timing and thresholds, demonstrates a resilience advantage, thereby enhancing the adaptability of the state estimation system in complex environments.

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#sentencerolethe authors' own workstates the main conclusionstrength
s0 As the number of heterogeneous redundant sensors on unmanned aerial vehicle (UAV) increases, onboard sensors require a more rational and efficient credibility evaluation system and a resilient fusion framework to achieve the essence of seamless sensor group switching. background 0.99 0.07 0.05 asserted 0.97
s1 A simple and efficient sensor credibility evaluation system is proposed to guide the selection of the optimal multi-source sensor submodel combination, thereby providing key model prior knowledge for multi-source resilient fusion. contribution 0.79 0.90 0.07 asserted 1.00
s2 Furthermore, a multi-model interactive resilient fusion framework based on RIEKF is proposed, utilizing the defined sensor credibility indexes to guide the design of the model transition probability matrix, thereby reducing the sensitivity of submodel weights to fusion stability and solving the problem of the model transition matrix lacking a basis for adjustment. method 0.59 0.90 0.12 asserted 1.00
s3 Model weights are updated in real time through credibility prior information and submodel posterior probabilities, thus leveraging the adaptive resilience advantage between models to achieve seamless switching between submodels in complex environments. method 0.97 0.75 0.14 asserted 1.00
s4 Experimental results show that the algorithm presented in this paper, without using any sensor fault diagnosis and isolation logic, without setting any complex detection timing and thresholds, demonstrates a resilience advantage, thereby enhancing the adaptability of the state estimation system in complex environments. result 0.94 0.95 0.79 asserted 1.00

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Every quoted sentence on this record is the authors'. Every label is from Pith's closed vocabulary, with the probability shown beside it. Every number in the measurements table is the authors', checked by code. Record as JSON

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Original abstract

As the number of heterogeneous redundant sensors on unmanned aerial vehicle (UAV) increases, onboard sensors require a more rational and efficient credibility evaluation system and a resilient fusion framework to achieve the essence of seamless sensor group switching. A simple and efficient sensor credibility evaluation system is proposed to guide the selection of the optimal multi-source sensor submodel combination, thereby providing key model prior knowledge for multi-source resilient fusion. Furthermore, a multi-model interactive resilient fusion framework based on RIEKF is proposed, utilizing the defined sensor credibility indexes to guide the design of the model transition probability matrix, thereby reducing the sensitivity of submodel weights to fusion stability and solving the problem of the model transition matrix lacking a basis for adjustment. Model weights are updated in real time through credibility prior information and submodel posterior probabilities, thus leveraging the adaptive resilience advantage between models to achieve seamless switching between submodels in complex environments. Experimental results show that the algorithm presented in this paper, without using any sensor fault diagnosis and isolation logic, without setting any complex detection timing and thresholds, demonstrates a resilience advantage, thereby enhancing the adaptability of the state estimation system in complex environments.

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Uses the method or tool of 1 paper
  • The system state $^(m_j)χ_k-1$ and error state covariance $^(m_j)P_k-1$ of the $j$th submodel Sensor measurements $^(i)Z_k$ in the $j$th submodel System state transition matrix $Φ_t,t+1$, predicted state covariance matrix $Q_0$, measurement covariance matrix $^(i)R_k$, noise excitation matrix $^(i)G_k$ The system state $^(m_j)χ_k$ and error state covariance $^(m_j)P_k$ of the $j$th submodel Sensor measurement residual statistic $^(i)q_k$ in the $j$th submodel Right-invariant error state one-step prediction: $dχ^R_t,t+1 ⟵Φ_t,t+1 dχ^R_t$ One-step covariance update: $P_t,t+1 ⟵Φ_t,t+1 P_t Φ_t,t+1^⊤+ G_0 Q_0 G_0^⊤$ Compute KF gain: $K_t+1 ⟵P_t,t+1 H^R,⊤_t+1(H^R_t+1 P_t,t+1 H^R,⊤_t+1 )^-1$ State update: $dχ^R_t+1 ⟵dχ^R_t,t+1 + K_t+1 (z_k - H^R_t+1 dχ^R_t,t+1 )$ Covariance update: $P_t+1 ⟵(I - K_t+1 H^R_t+1)P_t,t+1$ The Invariant Extended Kalman Filter (IEKF) algorithm has gained widespread att

    Semi-Aerodynamic Model Aided Invariant Kalman Filtering for UAV Full-State Estimation · Sensor Submodel Update Based on Right-Invariant Kalman Filter · 0.80

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