# Robust Self-Contained Pedestrian Navigation by Fusing the IMU and Compass Measurements via UFIR Filtering.

1. IntroductionIndoor pedestrian navigation (PN), which provides the position and the heading information of the target person in indoor environment, has received a topic [1, 2].

In order to provide the accurate position information of the person in indoor environment, many approaches have been proposed. For example, in [3, 4], the radio frequency identification (RFID)-based technologies have been proposed provide object self-localization. Yang and Shao and Ma et al. proposed in [5, 6] an autonomous positioning system operating on WiFi, which is also able to achieve the indoor localization in indoor environment. However, it should be pointed out that although the RFID- and WiFi-based methods mentioned above are able to provide the position information in indoor environment, the accuracy of such approaches is on meter-level. In order to improve the positioning accuracy, ultrasonic-based approaches are proposed in [7]. However, it should be pointed that although the ultrasonic-based approaches are on centimeter-level, it is easy to be outage. Meanwhile, the ultra wideband (UWB) technology [8] is employed in some approaches. For example, a location detection and tracking of moving targets by a 2D IR-UWB radar system is presented in [9]. It should be emphasized that the methods mentioned above have to employ extra infrastructures; moreover, the sampling time of these methods is larger [1,10].

In order to overcome the disadvantages of the methods mentioned above, the inertial navigation systems (INS) have been employed for providing the human position in global positioning system- (GPS-) denied areas. One of the famous examples is the navigation shoe proposed in [11], which employs the foot-mounted inertial measurement unit (IMU) to correct the error drift of the INS solution. Based on this model, there are many improving approaches. For example, in [12-14], the magnetic sensor is used to correct the positioning error of the foot-mounted IMU. On the other hand, there are also many approaches for the signal processing in INS. For example, the analysis for microelectromechanical system (MEMS) gyroscope within wide-temperature range is shown in [15].

Based on the INS, the Kalman filter (KF) and its improving methods are widely used to correct the INS solution error [16, 17]. However, despite great progress in the development of the KF approach, the recursive KF-based algorithms demonstrate good performance mostly when the noise statistics are known exactly, and the model perfectly matches the process; otherwise, the KF-based estimators often demonstrate poor performance [18-20]. In order to provide the robust estimation, the unbiased finite impulse response (UFIR) filter has been proposed in [21-23]. Then, there are some improving UFIR filters proposed to improve the performance [24-27]. Compared with the KF-based filters, UFIR filters just need the state vector size and the filtering horizon size, while ignoring the noise statistics [25, 28, 29].

In this paper, we propose a self-contained pedestrian navigation by fusing the IMU and compass measurements via UFIR filtering. To the self-contained pedestrian navigation scheme, the compass measurement is used to provide the accurate yaw to improve the accuracy of the attitude transformation matrix for the foot-mounted IMU solution. Moreover, we investigate the UFIR filter based on the self-contained pedestrian navigation scheme, which just needs the state vector size [M.sup.U] and the filtering horizon size [N.sup.U], while ignoring the noise statistics. Finally, a real test has been done to verify the performance of the proposed self-contained pedestrian navigation using the IMU and compass measurements via UFIR filter. The test results show that the proposed filter has robust performance compared with the KF. The remaining part of this paper is organized as follows. Section 2 designs the scheme of the self-contained pedestrian navigation using the IMU and compass measurements. Section 3 presents the UFIR algorithms for the self-contained pedestrian navigation. Testing and results are discussed in Section 4. Finally, Section 5 gives the conclusions.

2. The Self-Contained Pedestrian Navigation Using the IMU and Compass Measurements

In this section, the scheme of self-contained pedestrian navigation using the IMU and compass measurements will be designed. Then, the state and measurement equations based on the scheme which we designed will be investigated.

2.1. The Scheme of Self-Contained Pedestrian Navigation Using the IMU and Compass Measurements. In this subsection, we will introduce the scheme of self-contained pedestrian navigation using the IMU and compass measurements. The architecture of the self-contained pedestrian navigation employing the recent IMU and compass measurements is shown in Figure 1. In this work, we employ inertial measurement unit (IMU) and compass measurements for the indoor self-contained pedestrian navigation. The IMU is fixed on the shoe, and the compass is fixed on the shoulder. In this paper, the IMU is used to provide the acceleration a, angular velocity w, pitch, and the roll, which are used to compute the position and posture of the target person. Compared with the IMU fixed on the shoe, thigh, shank, and waist, the IMU fixed on the shoulder has the best performance for yaw measurement. Thus, we employ shoulder-mounted IMU to provide the yaw measurement for the solution, which can improve the accuracy of the attitude transformation matrix for the foot-mounted IMU solution. In theory, the true velocity of the pedestrian shoes should be zero when the shoe is on the floor (so called stance phase). Thus, the velocity measured from the foot-mounted IMU will be the error measurement of the velocity in the stance phase. And when the person is in a stance phase, the unbiased finite impulse response (UFIR) filter works; it employs the measurement of the velocity error derived from the foot-mounted IMU to estimate the INS position error; then, the INS solution is corrected by the error estimation.

Meanwhile, the body frame (so called b-frame) and the navigation frame (so called n-frame (East-North-Up, ENU)) used in this paper are also shown in this figure. Compared with the outdoor navigation, the area of the indoor self-contained pedestrian navigation is very small; thus, the earth's rotation is not considered in this paper.

2.2. The State and Measurement Equations for the UFIR Filter. In this subsection, the state and measurement equations for the UFIR filter will be designed. Based on the self-contained pedestrian navigation scheme proposed in Section 2.1, a UFIR filter with a 15-element vector will be introduced in this paper. The state equation of the UFIR filter used in this paper at time step tt is listed as

[mathematical expression not reproducible], (1)

where [[[[phi].sup.(n).sub.tt], [delta][V.sup.(n).sub.tt]].sup.T] denotes attitude and velocity error vectors in n-frame at time step tt and [[[[nabla].sup.(b).sub.tt], [[epsilon].sup.(b).sub.tt]].sup.T] denotes the biases for accelerometers and gyroscopes in b-frame at time step tt, respectively. All these 5 components mentioned above have 3 elements each:

[mathematical expression not reproducible]; (2)

here, [[a.sup.(n).sub.Ett] [a.sup.(n).sub.Ntt] [a.sup.(n).sub.Dtt]] is the acceleration in n-frame (East-North-Up, ENU) at time step tt; T denotes the sampling time; [[omega].sub.tt] is a system noise at time step tt with the covariance [Q.sub.tt].

Algorithm 1: Kalman filter algorithm for the self-contained scheme. Data: [Z.sub.tt], [X.sub.0], [P.sub.0], Q, [R.sub.tt] Result: [[??].sub.tt] (1) begin (2) for tt = 1: [infinity] do (3) [[??].sub.tt|tt-1] = [A.sub.tt][[??].sub.tt-1] (4) [P.sub.tt|tt-1] = [A.sub.tt-1][P.sub.tt-1] [A.sup.T.sub.tt] + Q (5) [K.sub.tt] = [P.sub.tt|tt-1][H.sup.T.sub.tt] [([H.sub.k][P.sub.tt|tt-1][H.sup.T.sub.tt] + [R.sub.tt]).sup.-1] (6) [mathematical expression not reproducible] (7) [P.sub.tt] = (I - [K.sub.tt][H.sub.tt])[P.sub.tt|tt-1] (8) end for (9) end

The measurement equation is listed in

[mathematical expression not reproducible], (3)

where [delta][[??].sup.(n).sub.tt] is the observations for the velocity error in n-frame at time step tt; [[eta].sub.tt] is a measurement noise with covariance is [R.sub.tt].

3. UFIR Algorithms for the Self-Contained Pedestrian Navigation

In this section, the KF and the UFIR filter for the indoor self-contained pedestrian navigation based on the scheme proposed in Section 2.1 will be discussed.

3.1. KF Algorithm. As one of the most used data fusion algorithm, the Kalman filter (KF) and its improving methods have been widely used in many fields [30-34]. And its pseudo code is listed as Algorithm 1. It should be pointed out that the Kalman filter and its improving methods need the accurate model description and noise description, especially the accurate Q and [R.sub.tt], to maintain the performance. However, it is not easy to get the information mentioned above in someplace.

Algorithm 2: UFIR filter algorithm for the self-contained scheme. Data: [Z.sub.tt], [M.sup.U], [N.sup.U] Result: [[??].sub.tt] (1) begin (2) for tt = [N.sup.U] : [infinity] do (3) m = tt - [N.sup.U] + 1, s = m + [M.sup.U] - 1 (4) [mathematical expression not reproducible] (5) [A.sup.t.sub.s,0] = [A.sub.s][A.sub.s-1] ... [A.sub.m+1] (6) [G.sub.s] = [A.sup.t.sub.s,0] [([H.sup.T.sub.s,m] [H.sub.s,m]).sup.-1][([A.sup.t.sub.s,0]).sup.T] (7) if tt = N then (8) [Z.sub.s,m] = [[[Z.sup.T.sub.m+3] [Z.sup.T.sub.m+2] [Z.sup.T.sub.m+1] [Z.sup.T.sub.m].sup.T] (9) [[??].sub.s] = [A.sub.s,0][([H.sup.T.sub.s,m] [H.sub.s,m]).sup.-1][H.sup.T.sub.s,m][Z.sup.T.sub.s,m] (10) end if (11) if tt > N then (12) [mathematical expression not reproducible] (13) end if (14) for kk = s + 1 : tt do (15) [mathematical expression not reproducible] (16) [G.sub.kk] = [[[H.sup.T.sub.kk][H.sub.kk] + [([A.sub.kk][G.sub.kk-1][A.sup.T.sub.kk]).sup.-1]].sup.-1] (17) [K.sub.kk] = [G.sub.kk][H.sub.kk] (18) [mathematical expression not reproducible] (19) end for (20) [mathematical expression not reproducible] (21) end for (22) end (23) [dagger] [M.sup.U] is the state vector size (24) [dagger] [N.sup.U] is the filtering horizon size

3.2. UFIR Filtering Algorithm. Compared with KF, the UFIR filter does not need the accurate Q and [R.sub.k] to keep its accuracy [26, 35]. Based on the self-contained scheme proposed in Section 2.1, the UFIR filtering algorithm is listed in Algorithm 2. Thus, we can say that the UFIR filter is more robust than the KF filter.

4. Test and Discussion

In this paper, we employ a real indoor test to verify the performance of the proposed self-contained pedestrian navigation using the IMU and compass measurements via UFIR filter. The real test was done in the Machine Building of the University of Jinan, Jinan, China. In this section, the real test will be designed and we will investigate the corresponding results. Firstly, the real test will be designed. Then, the performances of the KF and UFIR filter will be compared.

4.1. Setting. The test platform used in the real test consists of one 9 degree of freedom (DOF) IMU, one compass, one computer, and one encoder. The 9-DOF IMU is fixed on the shoe; it employs ADXL203, ADXRS620, and HMC5983 as accelerometer, gyroscope, and magnetometer, respectively, which is able to provide the human position. Then, one HMC5983-based compass which is fixed on the shoulder is used to provide more accurate yaw measurement, which helps improve the accuracy of the yaw for the foot-mounted IMU. The computer is used to collect the sensor data. The encoder used in the real test is able to provide the reference velocity of the person. The sampling time T used in (1) is 0.03 s. From Algorithm 2, we can see that the performance of the UFIR filter is just need [M.sup.U] and [N.sup.U]. From (1), we can get that [M.sup.U] = 12 and we employ [N.sup.U] = 13 in this paper. The prototype of the test platform is shown in Figure 2.

4.2. The Performance of the UFIR Filter. The position error of the UFIR filter for self-contained pedestrian navigation using the IMU and compass measurements will be discussed in this section. In this subsection, we employ two groups of parameters which listed in Table 1. 1

(1) INS Position Errors-Group 1. Trajectories measured by INS + ZUPT + KF and INS + ZUPT + UFIR for the first group of possible parameters (Group 1) are shown in Figures 3 and 4. From the figures, firstly, we can see that the proposed self-contained pedestrian navigation scheme is able to provide the person position without any auxiliary equipment. Secondly, we can see that the trajectories estimated by the KF and the UFIR filter are similar.

The absolute average position errors by the KF and UFIR filter in Test 1 (Group 1) are listed in Table 2. From the table, we can see that the position errors of the KF and UFIR filter are similar. Thus, we can see that the performances of KF and UFIR filter are similar in Test 1 (Group 1).

(2) INS Position Errors-Group 2. We now repeat the experiment for the second group of possible parameters (Group 2). The trajectories measured from UWB only model using least square algorithm and the INS/UWB loosely coupled integrated model using the KF and UFIR filter for the second group of possible parameters (Group 2) are shown in Figures 5 and 6. And the absolute average position errors by the KF and UFIR filter in Test 2 (Group 2) are listed in Table 3. From the figures, we can see easily that the KF has been diverged, while the performance of the UFIR filter is still good.

5. Conclusion

In this paper, a self-contained pedestrian navigation by fusing the IMU and compass measurements via UFIR filtering and both the implement and test are proposed. To the self-contained pedestrian navigation scheme, the compass measurement is used to provide the accurate yaw to improve the accuracy of the attitude transformation matrix for the foot-mounted IMU solution. Moreover, we investigate the UFIR filter based on the self-contained pedestrian navigation scheme, which just needs the state vector size [M.sup.U] and the filtering horizon size [N.sup.U], while ignoring the noise statistics. Finally, a real test has been done to verify the performance of the proposed self-contained pedestrian navigation using the IMU and compass measurements via UFIR filter. The test results show that the proposed filter has robust performance compared with the KF.

https://doi.org/10.1155/2018/8401967

Conflicts of Interest

The authors declare no conflicts of interest.

Acknowledgments

This work was supported in part by the China Postdoctoral Science Foundation (no. 2017M622204) and the Doctoral Foundation of the University of Jinan (no. XBS1503).

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Meng Hou [ID], (1) Yuan Xu, (2) and Xiao Liu (1)

(1) School of Electrical Engineering and Automation, Qilu University of Technology, Jinan 250353, China

(2) The School of Electrical Engineering, University of Jinan, Jinan 250022, China

Correspondence should be addressed to Meng Hou; houmeng@qlu.edu.cn

Received 31 January 2018; Revised 17 March 2018; Accepted 26 March 2018; Published 8 May 2018

Academic Editor: Choon Ki Ahn

Caption: Figure 1: The architecture of the self-contained pedestrian navigation using the IMU and compass measurements.

Caption: Figure 2: The prototype of the test platform.

Caption: Figure 3: Trajectory measured by INS + ZUPT + KF for the first group of possible parameters (Group 1).

Caption: Figure 4: Trajectory measured by INS + ZUPT + UFIR for the first group of possible parameters (Group 1).

Caption: Figure 5: Trajectory measured by INS + ZUPT + KF for the second group of possible parameters (Group 2).

Caption: Figure 6: Trajectory measured by INS + ZUPT + UFIR for the second group of possible parameters (Group 2).

Table 1: The parameters for the tests. [X.sub.0] [P.sub.0] Q Group 1 [0.sub.12x1] [I.sub.2x12] [I.sub.2x12] Group 2 [0.sub.12x1] [I.sub.2x12] [10.sup.-12][I.sub.12x12] R [N.sup.U] Group 1 [I.sub.3x3] 13 Group 2 [I.sub.3x3] 13 Table 2: Absolute average position errors by different filters in Test 1 (Group 1). Absolute average position errors [m] Model East direction North direction KF 0.25 0.29 UFIR 0.22 0.31 Table 3: Absolute average position errors by different filters in Test 2 (Group 2). Absolute average position errors [m] Model East direction North direction KF 0.88 2.79 UFIR 0.22 0.31

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Title Annotation: | Research Article |
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Author: | Hou, Meng; Xu, Yuan; Liu, Xiao |

Publication: | Journal of Electrical and Computer Engineering |

Date: | Jan 1, 2018 |

Words: | 3960 |

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