2014
DOI: 10.2514/1.g000460
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Observability-Based Optimal Sensor Placement for Flapping Airfoil Wake Estimation

Abstract: This work considers the optimal sensor placement problem for a general nonlinear system using the eigenvalues of the observability Gramian in the cost function. The problem is formulated as a mixed-integer convex optimization problem. Using the empirical observability Gramian, the input data to this optimization problem are computed from a simulation of the nonlinear system with no analytical model required. A piecewise linear approximation to the observability Gramian is proposed using special ordered sets of… Show more

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Cited by 23 publications
(17 citation statements)
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References 36 publications
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“…Method 1 ( 2 -Optimal Sensor Combination). Solve for N s , P = P T > 0, 12 , Z = Z T > 0, and ∈ ℝ >0 that minimize subject to (13), (14), (15), (16), and tr(Z) < 1.…”
Section: Sensor Combination Methodsmentioning
confidence: 99%
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“…Method 1 ( 2 -Optimal Sensor Combination). Solve for N s , P = P T > 0, 12 , Z = Z T > 0, and ∈ ℝ >0 that minimize subject to (13), (14), (15), (16), and tr(Z) < 1.…”
Section: Sensor Combination Methodsmentioning
confidence: 99%
“…The  ∞ -optimal combination of the sensor measurements is presented in the following method. 12 , and ∈ ℝ >0 that minimize subject to (13), (17), and (18).…”
Section: Sensor Combination Methodsmentioning
confidence: 99%
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“…Sensor placement optimization for observability was first suggested in Ref. 36, and has subsequently been studied for a wide range of applications such as structural vibration, 37 chemical reactors, 38 airfoil wake estimation, 39 and Mars entry navigation. 40 Another approach, suggested in Ref.…”
Section: A Port Placement Optimizationmentioning
confidence: 99%
“…With the majority of the sensilla placed proximally, they are also more protected from degraded observability owing to wing damage (e.g. [59]) although the more distal sensilla at the trailing edge are informative for fine-scale control of aerodynamic loads at that location [10,60]. …”
Section: Wing Deformation and How To Sense Aeroelasticitymentioning
confidence: 99%