Position, Navigation, and Timing Technologies in the 21st Century

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Covers the latest developments in PNT technologies, including integrated satellite navigation, sensor systems, and civil applications Featuring sixty-four chapters that are divided into six parts, this two-volume work provides comprehensive coverage of the state-of-the-art in satellite-based position, navigation, and timing (PNT) technologies and civilian applications. It also examines alternative navigation technologies based on other signals-of-opportunity and sensors and offers a comprehensive treatment on integrated PNT systems for consumer and commercial applications.
Volume 1 of
contains three parts and focuses on the satellite navigation systems, technologies, and engineering and scientific applications. It starts with a historical perspective of GPS development and other related PNT development. Current global and regional navigation satellite systems (GNSS and RNSS), their inter-operability, signal quality monitoring, satellite orbit and time synchronization, and ground- and satellite-based augmentation systems are examined. Recent progresses in satellite navigation receiver technologies and challenges for operations in multipath-rich urban environment, in handling spoofing and interference, and in ensuring PNT integrity are addressed. A section on satellite navigation for engineering and scientific applications finishes off the volume.
Volume 2 of
consists of three parts and addresses PNT using alternative signals and sensors and integrated PNT technologies for consumer and commercial applications. It looks at PNT using various radio signals-of-opportunity, atomic clock, optical, laser, magnetic field, celestial, MEMS and inertial sensors, as well as the concept of navigation from Low-Earth Orbiting (LEO) satellites. GNSS-INS integration, neuroscience of navigation, and animal navigation are also covered. The volume finishes off with a collection of work on contemporary PNT applications such as survey and mobile mapping, precision agriculture, wearable systems, automated driving, train control, commercial unmanned aircraft systems, aviation, and navigation in the unique Arctic environment.
In addition, this text:
Serves as a complete reference and handbook for professionals and students interested in the broad range of PNT subjects Includes chapters that focus on the latest developments in GNSS and other navigation sensors, techniques, and applications Illustrates interconnecting relationships between various types of technologies in order to assure more protected, tough, and accurate PNT
will appeal to all industry professionals, researchers, and academics involved with the science, engineering, and applications of position, navigation, and timing technologies.pnt21book.com

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Finally, the collection of particle weights can be normalized via

(36.110) Position Navigation and Timing Technologies in the 21st Century - изображение 136

then Eq. 36.109becomes

(36.111) which we will exploit to develop a recursive estimator 3638 Sequential - фото 137

which we will exploit to develop a recursive estimator.

36.3.8 Sequential Importance Sampling Recursive Estimator

In this section, we leverage the previously presented concept of importance sampling to derive the basis for a recursive nonlinear estimator using Monte Carlo integration [4]. This type of filter is generally referred to as a recursive particle filter.

Consider the following general system model:

(36.112) Position Navigation and Timing Technologies in the 21st Century - изображение 138

(36.113) Position Navigation and Timing Technologies in the 21st Century - изображение 139

where x kis the state vector at time k , f(·, ·) is the process model function at time k – 1, w k − 1is the process noise vector, h(·, ·) is the observation function, and v kis the measurement noise vector at time k . The noise vectors are assumed to be independent of each other and in time with a known density function. Note that Gaussian densities are not required or assumed.

Assuming we begin with a known posterior density, p ( x k − 1| ℤ k − 1). If N samples are drawn from an associated proposal density,

(36.114) With normalized weights given by 36115 where κ is the normalization factor - фото 140

With normalized weights given by

(36.115) where κ is the normalization factor required such that the sum of weights is - фото 141

where κ is the normalization factor required such that the sum of weights is unity, the posterior density function is expressed by the collection of particles and weights

(36.116) or equivalently 36117 Our goal is to estimate the posterior density at - фото 142

or, equivalently

(36.117) Our goal is to estimate the posterior density at time k p x k ℤ k by - фото 143

Our goal is to estimate the posterior density at time k , p ( x k| ℤ k), by incorporating the statistical process model and the observation at time k . The density function of interest can be written as

(36.118) 36119 Assuming our proposal density can be factored 36120 - фото 144

(36.119) Assuming our proposal density can be factored 36120 the posterior - фото 145

Assuming our proposal density can be factored:

(36.120) Position Navigation and Timing Technologies in the 21st Century - изображение 146

the posterior particle locations can be sampled from

(36.121) Position Navigation and Timing Technologies in the 21st Century - изображение 147

Thus, the associated particle weights at time k can be calculated in a similar fashion as Eq. 36.108:

(36.122) Substituting Eqs 36119and 36120into Eq 36122yields 36123 Note that - фото 148

Substituting Eqs. 36.119and 36.120into Eq. 36.122yields

(36.123) Note that this equation is a function of the posterior weights at time k 1 - фото 149

Note that this equation is a function of the posterior weights at time k – 1; thus, the right‐hand fraction of Eq. 36.123can be replaced according to Eq. 36.108, which yields the final particle weight update equation from time k – 1 to time k :

(36.124) which can be normalized such that the collection of weights sums to one thus - фото 150

which can be normalized such that the collection of weights sums to one, thus approximating the posterior density as

(36.125) In this manner the particle locations and weights can be continuously - фото 151

In this manner, the particle locations and weights can be continuously maintained and updated using a recursive estimation framework.

36.3.9 Sampling Particle Filter Demo

In this section, we apply a sequential importance sampling particle filter design to our previous nonlinear estimation example. As before, an identical, randomly generated trajectory and measurement set from the MMAE example ( Section 36.3.3) are used as inputs to the filter. Once again, for reference, the system parameters are specified in Table 36.1, and the resulting trajectory, range observations, and phase observations are shown in Figure 36.3. For this example, we use 10 000 two‐dimensional particles. Finally, we exercise an importance resampling procedure [6] to ensure that the number of effective particles remains acceptable.

The SIS particle filter global state estimate and density function of position after one observation ( t = 1 s) are shown in Figure 36.17. In this example, we show the location of the particles along with the estimated mean and one‐sigma standard deviation calculated using the ensemble of particles. In the figures below, the estimated mean is represented as a magenta “plus,” the true state is a green asterisk, and the estimated 2‐sigma error bounds as a dashed ellipse. Each particle location is shown as a black dot.

After 22 cycles, the density shows a reduced number of peaks (see Figure 36.18) and is clearly multi‐modal. Based on our knowledge of the true density functions developed in the previous examples, this indicates that the filter is incorporating sensor observations and the statistical dynamics model to effectively eliminate a number of potential ambiguity possibilities.

After 100 cycles ( Figure 36.19), the filter has converged to a single ambiguity.

Figure 3617 SIR particle filter initial state estimate and position density - фото 152

Figure 36.17 SIR particle filter initial state estimate and position density function. Note that the density function is extremely multi‐modal due to the limited information available at this point.

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