Pages that link to "Item:Q4905770"
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The following pages link to Initial alignment for nonlinear inertial navigation systems with multiple disturbances based on enhanced anti-disturbance filtering (Q4905770):
Displaying 10 items.
- Realization of an autonomous integrated suite of strapdown astro-inertial navigation systems using unscented particle filtering (Q1029857) (← links)
- Robust \(H_\infty\)-correction of three-component inertial navigation systems (Q1386905) (← links)
- Unbiased information filtering for systems with missing measurement based on disturbance estimation (Q1660982) (← links)
- Novel SINS initial alignment method under large misalignment angles and uncertain noise based on nonlinear filter (Q1992914) (← links)
- Robust particle filtering with enhanced outlier resilience and real-time disturbance compensation (Q2656882) (← links)
- Velocity and position error compensation using strapdown inertial navigation system/celestial navigation system integration based on ensemble neural network (Q2853510) (← links)
- (Q3582792) (← links)
- Minimal order time sharing filters for INS in-flight alignment (Q3959853) (← links)
- Composite predictive flight control for airbreathing hypersonic vehicles (Q5499804) (← links)
- Fixed‐time event‐triggered controller of a state‐constrained nonlinear system: A zero‐error tracking control approach (Q6194770) (← links)
