Abstract
A promising line of research attempts to bridge the gap between a detector and a tracker by means of considering jointly optimal parameter settings for both of these subsystems. Along this fruitful path, this chapter focuses on the problem of detection threshold optimization in a tracker-aware manner so that a feedback from the tracker to the detector is established to maximize the overall system performance. Special emphasis is given to the optimization schemes based on two non-simulation performance prediction techniques for the probabilistic data association filter, namely, the modified Riccati equation (MRE) and the hybrid conditional averaging algorithm. The possible improvements are presented in non-maneuvering target tracking where a number of algorithmic and experimental evaluation gaps are identified and newly proposed methods are compared with the existing ones in a unified theoretical and experimental framework. Furthermore, for the MRE-based dynamic threshold optimization problem, a closed-form solution is proposed. This solution brings a theoretical lower bound on the operating signal-to-noise ratio concerning when the tracking system should be switched to the track-before-detect mode.
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Notes
- 1.
This includes the processing blocks prior to detection such as analog-to-digital (A/D) conversion, beamforming, pulse compression, clutter filtering, and Doppler processing [57].
- 2.
This in turn determines the detector operating point (P FA,P D ) for a given SNR and hence the detection threshold.
- 3.
In this chapter, we consider only the detection threshold as our optimization variable. A more general set including also the transmitting waveform as in the case of cognitive radar [25] is out of the scope of the present chapter.
- 4.
See, e.g., [9, pp. 373].
- 5.
This in essence results in a feedback from the tracker to the detector as illustrated in Fig. 6.1.
- 6.
Examples of continuous uncertainties are the inaccuracy in the measurements and “small” perturbations in the target motion which are usually modeled as an additive measurement noise and process noise, respectively. These types of uncertainties are well-understood and solved in the literature over the past four decades under the title of classical state estimation [1, 9, 42]. However, major challenges of tracking arise from two discrete-valued uncertainties: measurement origin uncertainty, which is, in the words of Li and Bar-Shalom [46], the crux of tracking, and target maneuver which appears as an abrupt and “large” deviation in the target motion.
- 7.
In this chapter, we consider this aspect, i.e., tracker-aware optimization of detection thresholds.
- 8.
The common notation means that “the random variable x is normally (Gaussian) distributed with mean \(\bar{x}\) and covariance Σ.”
- 9.
The gate probability (P G ) is defined as the probability that the target-originated measurement falls inside the validation gate given that the target is detected.
- 10.
The measurement z(k) is said to be a validated measurement, if it is inside a validation gate defined in (6.3).
- 11.
This covers homogeneous and Gaussian background detector noise, a Swerling-I target fluctuation and square-law detection scheme. In the radar detection theory, such assumptions are made frequently when obtaining the ROC curves for a specific detector [65]. We refer to this joint assumption shortly as \(\mathrm{HOG_{I}^{SQL}}\).
- 12.
It can be argued that a decreasing value of N C , namely decreasing the number of resolution cells falling inside a validation gate, suggests that the gate volume (hence the Gaussian hyper-ellipse suggested by the filter covariance) is diminishing. This in turn suggests the convergence of the filter to its steady-state although this may not be guaranteed to be the correct state estimate. Conversely, by the same argument, a large value of N C suggests a large gate volume, which in turn suggests that the filter is comparatively in its transient phase.
- 13.
Normally, a 2D radar provides polar measurements. A rectangular resolution cell is adopted to have a linear measurement model.
- 14.
This is valid for a special case of a NP detector under \(\mathrm{HOG}_{\mathrm{I}}^{\mathrm{SQL}}\) assumption.
- 15.
This is an important practical problem in the radar. Under excessive number of false detections, the radar may initiate lots of false tracks. This causes the radar to allocate its resources, e.g., dwell time, transmission power, unnecessarily and inefficiently.
- 16.
Given an initial interval of uncertainty, [a,b] and the number of function evaluations, N, the Fibonacci Search algorithm reduces the length of the uncertainty interval to (b−a)/F N+1, where F N+1 is the (N+1)th number in the Fibonacci sequence {1,1,2,…}. Therefore, given the number N, the length of the final uncertainty interval, so the maximum error in finding the extremum point, is determined. Here, we do the other way around. That is, we specify the maximum error tolerance that we are required to have at the end of the algorithm which in turn determines the minimum required number of function evaluations, N.
- 17.
We accept that the track is lost for the ith Monte Carlo run if \(\varepsilon_{\mathrm{POS}}^{i}>\rho\) where \(\rho\triangleq\sqrt{\mathrm{tr}\{R\}}\) is the measurement error level and \(\varepsilon_{\mathrm{POS}}^{i}\) is the average position estimation error for the ith run.
- 18.
These measures can be seen also as transient vs. steady-state performance, respectively.
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Aslan, M.Ş., Saranlı, A. (2013). Joint Optimization of Detection and Tracking in Adaptive Radar Systems. In: Chatterjee, A., Nobahari, H., Siarry, P. (eds) Advances in Heuristic Signal Processing and Applications. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-37880-5_6
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