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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Discretizing the dynamics ( Eq. (38.1)) at a sampling interval T yields the discrete‐time‐equivalent model

where is a discretetime zeromean white noise sequence with covariance Q clk - фото 182

where is a discretetime zeromean white noise sequence with covariance Q clk and - фото 183is a discrete‐time zero‐mean white noise sequence with covariance Q clk, and

(38.2) Table 382 Typical h 0and h 2values for different OCXOs 36 Source J - фото 184

Table 38.2 Typical h 0and h −2values for different OCXOs [36]

Source: J. Curran, G. Lachapelle, and C. Murphy, “Digital GNSS PLL design conditioned on thermal and oscillator phase noise,” IEEE Transactions on Aerospace and Electronic Systems , vol. 48, no. 1, pp. 180–196, January 2012.

h 0 h −2
2.6 × 10 −22 4.0 × 10 −26
8.0 × 10 −20 4.0 × 10 −23
3.4 × 10 −22 1.3 × 10 −24

38.4 Navigation Frameworks in Cellular Environments

BTS positions can be readily obtained via several methods, for example, (i) from cellular BTS databases (if available) or (ii) by deploying multiple mapping receivers with knowledge of their own states, estimating the position states of the BTSs for a sufficiently long period of time [37–39]. These estimates are physically verifiable via surveying or satellite images. Unlike BTS positions, which are static, the clock error states are stochastic and dynamic, as discussed in Section 38.3, and are difficult to verify.

Estimating the BTSs’ states can be achieved via two frameworks:

Mapper/NavigatorThis framework comprises (i) receiver(s) with knowledge of their own states, referred to as mapper(s), making measurements on ambient BTSs (e.g. pseudorange and carrier phase). The mappers’ role is to estimate the cellular BTSs’ states. (ii) A receiver with no knowledge of its own states, referred to as the navigator, making measurements on the same ambient BTSs to estimate its own states, while receiving estimates of the BTSs’ states from the mappers.

Radio SLAMIn this framework, the receiver maps the BTSs simultaneously with localizing itself in the radio environment.

To make the estimation problems associated with the above frameworks observable, certain a priori knowledge about the BTSs’ or receiver’s states must be satisfied [27, 40–42]. For simplicity, a planar environment will be assumed, with the receiver and BTS three‐dimensional (3D) position states appropriately projected onto such a planar environment. The state of the receiver is defined as Position Navigation and Timing Technologies in the 21st Century - изображение 185, where Position Navigation and Timing Technologies in the 21st Century - изображение 186is the position vector of the receiver, δt ris the receiver’s clock bias, and c is the speed of light. Similarly, the state of the i ‐th BTS is defined as Position Navigation and Timing Technologies in the 21st Century - изображение 187, where Position Navigation and Timing Technologies in the 21st Century - изображение 188is the position vector of the i ‐th BTS, and Position Navigation and Timing Technologies in the 21st Century - изображение 189is its clock bias. The pseudorange measurement to the i ‐th BTS, ρ i, can be expressed as

(38.3) Position Navigation and Timing Technologies in the 21st Century - изображение 190

where and v iis the measurement noise which is modeled as a zeromean Gaussian - фото 191and v iis the measurement noise, which is modeled as a zero‐mean Gaussian random variable with variance картинка 192[27]. The following sections outline the calculations associated with each navigation framework assuming pseudorange measurements from cellular towers. Frameworks with carrier phase measurements are discussed in [43].

38.4.1 Mapper/Navigator Framework

Assuming that the receiver is drawing pseudoranges from N ≥ 3 BTSs with known states, the receiver’s state can be estimated from ( Eq. (38.3)) by solving a weighted nonlinear least‐squares (WNLS) problem. However, in practice, the BTSs’ states are unknown , in which case the mapper/navigator framework can be employed [18, 25].

Consider a mapper with knowledge of its own state vector (by having access to GNSS signals, for example) to be present in the navigator’s environment as depicted in Figure 38.3.

The mapper’s objective is to estimate the BTSs’ position and clock bias states and share these estimates with the navigator through a central database. For simplicity, assume the position states of the BTSs to be known and stored in a database. In the sequel, it is assumed that the mapper is producing an estimate картинка 193and an associated estimation error variance картинка 194for each of the BTSs.

Consider M mappers and N BTSs. Denote the state vector of the j ‐th mapper by картинка 195, the pseudorange measurement by the j ‐th mapper on the i‐ th BTS by картинка 196, and the corresponding measurement noise by картинка 197. Assume картинка 198to be independent for all i and j with a corresponding variance Define the set of measurements made by all mappers on the i th BTS as - фото 199. Define the set of measurements made by all mappers on the i ‐th BTS as

Figure 383 Mapper and navigator in a cellular environment Khalife et al - фото 200

Figure 38.3 Mapper and navigator in a cellular environment (Khalife et al. [18]; Khalife and Kassas [25]).

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