Rapid Transfer Alignment in the Presence of Time Correlated Measurement and System Noise

Wendel, Jan; Metzger, Jürgen; Trommer, Gert F.

doi:10.2514/6.2004-4778

Cited by 15 publications

(12 citation statements)

References 1 publication

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“…Substituting the term on the right-hand side of (55) into (53) and using (38) in Lemma 2.2, we obtain P n xx;kjk…”

Section: Sufficient Conditions For H1-sgqkf Stochastic Boundedness Ofmentioning

confidence: 98%

“…So TA performance represents the primary challenge in modeling uncertainty. Four distinctive approaches to treat the aircraft flexibilities and vibrations in TA are: determining the in-flight flexible aircraft wing motion using various measurement techniques [37], and processing the flexibilities and vibrations sensed by the inertial sensors as system noise in the filer equations [38]. The first three approaches above need extra hardware or software expenditures, the last one needs only software expenditures.…”

Section: The H1 Sgqkf Application In Transfer Alignmentmentioning

confidence: 99%

See 1 more Smart Citation

Robust stability analysis of H∞-SGQKF and its application to transfer alignment

et al. 2015

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“…Substituting the term on the right-hand side of (55) into (53) and using (38) in Lemma 2.2, we obtain P n xx;kjk…”

Section: Sufficient Conditions For H1-sgqkf Stochastic Boundedness Ofmentioning

confidence: 98%

Section: The H1 Sgqkf Application In Transfer Alignmentmentioning

confidence: 99%

Robust stability analysis of H∞-SGQKF and its application to transfer alignment

et al. 2015

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“…In 1997, Shortelle et al did an experiment on rapid transfer alignment in F-16 [5]. The expe-rimental results showed that the velocity plus attitude match method could reach a attitude precision less than 1 mrad in 10 s. From [6][7][8][9][10][11][12][13], we can see that the method was successfully applied to many elds. In recent years, transfer alignment technology has made a signi cant development.…”

Section: Introductionmentioning

confidence: 96%

Rapid transfer alignment for SINS of carrier craft

Wang

Xiao

2013

J. of Syst. Eng. Electron.

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In order to improve the survival ability and rapid response ability of the carrier craft, a new rapid transfer alignment method of the strapdown inertial navigation system (SINS) on a rocking base is put forward. In the method, the aircraft carrier does not need any form of movement. Meantime, interfering motions such as rolling, pitching, and yawing motions caused by sea waves are effectively used. Firstly, the deck exure deformation model is made. Secondly, the state space model of transfer alignment is presented. Finally, the feasibility of this method is validated by the simulation. Simulation results show that the misalignment angle error can be estimated and reach an anticipated precision-0.2 mrad in 5 s, while the deck deformation angle error can be estimated and reach a better precision-0.1 mrad in 20 s.

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“…As pointed out (Britting, 1971;Itzhack and Porat, 1980;Yi, 1987 andWendel et al, 2004), the accelerometer and gyro instrument error parameterization is very complex for accurate modelling. However, most literatures consider the random error of gyros as a mixture of three independent elements that will be referred to hereafter as successive start drifting ε bi , random walk ε ri and white noise signals w g .…”

Section: P Ro B L E M Fomentioning

confidence: 99%

“…Rhee expanded the instantaneous observability results to the integrated INS/Global Positioning System (GPS) system in (Rhee et al, 2004). In the presence of time correlated noise, Wendel presented a rapid TA scheme (Wendel et al, 2004) where the full observability was achievable with brief Wing Rock (WR) manoeuvres. In order to excite azimuth-related states to extreme magnitude, Efraim proposed a new in-drilling alignment procedure (Efraim and Mintchev, 2007a;2007b).…”

Section: Introduction Inertial Navigation System (Ins)mentioning

confidence: 99%

Performance Enhancement of Large-Ship Transfer Alignment: A Moving Horizon Approach

Yang

Wang

et al. 2012

J. Navigation

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In shipborne Transfer Alignment (TA) applications, partial observability is one of the most important factors limiting convergence velocity. This paper proposes a new method of attributing weak observable states and lever-arm variables to a group of constraints in order to improve the observability of TA model. This yields the so-called Constrained Transfer Alignment (CTA) model which is uniformly observable even under zero-manoeuvre conditions. Within this framework, the Moving Horizon Estimation (MHE) and its stability analysis are also addressed. Finally, comparative simulation results are given to demonstrate the advantages of the proposed approach.

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Rapid Transfer Alignment in the Presence of Time Correlated Measurement and System Noise

Cited by 15 publications

References 1 publication

Robust stability analysis of H∞-SGQKF and its application to transfer alignment

Robust stability analysis of H∞-SGQKF and its application to transfer alignment

Rapid transfer alignment for SINS of carrier craft

Performance Enhancement of Large-Ship Transfer Alignment: A Moving Horizon Approach

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