2009 European Control Conference (ECC) 2009
DOI: 10.23919/ecc.2009.7075024
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Pose observers for Unmanned Air Vehicles

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Cited by 5 publications
(7 citation statements)
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“…From there the proposed observer is given by (10) and (16) withγ defined by (12) and with the innovation terms σ ξ , σ R , σ V , σ Q,1 and σ Q,2 determined from the input u calculated according to (8) and (9) with the matricesQ(t) andV(t) chosen larger than some positive matrices.…”
Section: Assumptionmentioning
confidence: 99%
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“…From there the proposed observer is given by (10) and (16) withγ defined by (12) and with the innovation terms σ ξ , σ R , σ V , σ Q,1 and σ Q,2 determined from the input u calculated according to (8) and (9) with the matricesQ(t) andV(t) chosen larger than some positive matrices.…”
Section: Assumptionmentioning
confidence: 99%
“…According to [11,Corollary 3.2] and Lemma 2, good conditioning of the solutions P(t) to the continuous Riccati equation (9) and exponential stability of the proposed observer rely on the uniform observability of the pair (A (t), C (t)) obtained by setting x = 0 in the expressions of the matrices A and C derived previously. In view of (22) one has…”
Section: Observability and Stability Analysismentioning
confidence: 99%
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