Vision-based adaptive guidance law for intercepting a manoeuvring target
Vision-based adaptive guidance law for intercepting a manoeuvring target
- Author(s): Y. Tian ; Y. Li ; Z. Ren
- DOI: 10.1049/iet-cta.2010.0092
For access to this article, please select a purchase option:
Buy article PDF
Buy Knowledge Pack
IET members benefit from discounts to all IET publications and free access to E&T Magazine. If you are an IET member, log in to your account and the discounts will automatically be applied.
Thank you
Your recommendation has been sent to your librarian.
- Author(s): Y. Tian 1, 2 ; Y. Li 2 ; Z. Ren 1
-
-
View affiliations
-
Affiliations:
1: School of Automation Science and Electrical Engineering, Beijing University of Aeronautics and Astronautics, Beijing, People's Republic of China
2: School of Surveying and Spatial Information Systems, University of New South Wales, Sydney, Australia
-
Affiliations:
1: School of Automation Science and Electrical Engineering, Beijing University of Aeronautics and Astronautics, Beijing, People's Republic of China
- Source:
Volume 5, Issue 3,
17 February 2011,
p.
421 – 428
DOI: 10.1049/iet-cta.2010.0092 , Print ISSN 1751-8644, Online ISSN 1751-8652
- « Previous Article
- Table of contents
- Next Article »
This article introduces an adaptive guidance law for intercepting a manoeuvring target using information from an imaging seeker. The relative missile–target kinematics is represented in the line-of-sight (LOS) frame, and the image information – instead of the relative range – is introduced to formulate the interception problem as an adaptive control problem with an unknown control coefficient. Considering the target's acceleration as a time-varying bounded external disturbance, an estimator with an adaptive property is derived. It is proven that the proposed guidance law can guarantee the LOS angular rates global uniform ultimate boundedness during the terminal course. The effectiveness of the proposed guidance law has been demonstrated in simulations for two kinds of typical manoeuvring targets.
Inspec keywords: adaptive control; object detection; computer vision; missile guidance
Other keywords:
Subjects: Aerospace control; Military control systems; Optical, image and video signal processing; Military detection and tracking systems; Computer vision and image processing techniques; Self-adjusting control systems
References
-
-
1)
- Z. Ding . Universal disturbance rejection for nonlinearsystems in output feedback form. IEEE Trans. Autom. Control , 7 , 1222 - 1227
-
2)
- Cao, C., Hovakimyan, N.: `L1 adaptive controller for nonlinear systems in the presence of unmodelled dynamics: part II', American Control Conf., 2008, Seattle, WA, p. 4099–4104.
-
3)
- V. Stepanyan , N. Hovakimyan . Visual tracking of a maneuvering target. J. Guid. Control Dyn. , 1 , 66 - 80
-
4)
- P. Zarchan . Tactical and strategic missile guidance. Prog. Astronaut. Aeronaut. , 95 - 118
-
5)
- R.D. Nussbaum . Some remarks on the conjecture in parameter adaptive control. Syst. Control Lett. , 3 , 243 - 246
-
6)
- F. Hong , S.S. Ge , B. Ren , T.H. Lee . Robust adaptive control for a class of uncertain strict-feedback nonlinear systems. Int. J. Robust Nonlinear Control , 7 , 746 - 767
-
7)
- T.L. Song , T.Y. Um . Practical guidance for homing missiles with bearings-only measurements. IEEE Trans. Aerosp. Electron. Syst. , 1 , 434 - 443
-
8)
- Wang, J.: `Robust adaptive control of a class of nonlinearly parameterized time-varying uncertain systems', Am. Control Conf., 2009, St. Louis, MO, p. 1940–1945.
-
9)
- J.-B. Pomet , L. Praly . Adaptive nonlinear regulation: estimation from the Lyapunov equation. IEEE Trans. Autom. Control , 6 , 729 - 740
-
10)
- S.S. Ge , J. Wang . Robust adaptive tacking for time-varying uncertain nonlinear systems with unknown control coefficients. IEEE Trans. Autom. Control , 8 , 1463 - 1469
-
11)
- Ge, S.S., Wang, J.: `Robust adaptive stabilization for time varying uncertain nonlinear systems with unknown control coefficients', Proc. 41st IEEE Conf. Decision and Control, 10–13 December 2002, Las Vegas, NV, p. 3952–3957.
-
12)
- C. Cao , N. Hovakimyan , J. Wang . Intelligent excitation for adaptive control with unknown parameters in reference input. IEEE Trans. Autom. Control , 8 , 1525 - 1532
-
13)
- J. Ben-asher , I. Yaesh . Advances in missile guidance theory. Prog. Astronaut. Aeronaut. , 89 - 126
-
14)
- T.L. Song . Observability of target tracking with bearings-only measurements. IEEE Trans. Aerosp. Electron. Syst. , 4 , 1468 - 1472
-
15)
- V. Stepanyan , N. Hovakimyan . Adaptive disturbance rejection controller for visual tracking of a maneuvering target. J. Guid. Control Dyn. , 4 , 1090 - 1106
-
16)
- X.D. Ye , J.P. Jiang . Adaptive nonlinear design without a priori knowledge of control directions. IEEE Trans. Autom. Control , 11 , 1617 - 1621
-
17)
- Y. Zhang , S.J. Qin . Adaptive actuator fault compensation for linear systems with matching and unmatching uncertainties. J. Process Control , 9 , 985 - 990
-
18)
- Y. Zhang , S.J. Qin . Adaptive actuator/component fault compensation for nonlinear system. AIChE J. , 9 , 2404 - 2412
-
19)
- V.J. Aidala , S. Hammel . Utilization of modified polar coordinates for bearings-only tracking. IEEE Trans. Autom. Control , 3 , 283 - 294
-
20)
- C. Cao , N. Hovakimyan . L1 adaptive controller for systems with unknown time-varying parameters and disturbances in the presence of non-zero trajectory initialization error. Int. J. Control , 7 , 1147 - 1161
-
21)
- K.R. Babu , I.G. Sarma , K.N. Swamy . Switched bias proportional navigation for homing guidance against highly maneuvering target. J. Guid. Control Dyn. , 6 , 1357 - 1363
-
22)
- X. Ye , Z. Ding . Robust tracking control of uncertain nonlinear systems with unknown control directions. Syst. Control Lett. , 1 , 1 - 10
-
23)
- Cao, C., Hovakimyan, N.: `Vision-based aerial tracking using intelligent excitation', Proc. American Control Conf., 8–10 June 2005, Portland, OR, p. 5091–5096.
-
24)
- Cao, C., Hovakimyan, N.: `Guaranteed transient performance with L1 adaptive controller for systems with unknown time-varying parameters and bounded disturbances: part I', American Control Conf., 2008, Seattle, WA, p. 4093–4098.
-
25)
- Betser, A., Vela, P., Tannenbaum, A.: `Automatic tracking of flying vehicles using geodesic snakes and Kalman filtering', Proc. IEEE Conf. Decision and Control, 14–17 December 2004, Paradise Island, Bahamas, p. 1649–1654.
-
26)
- X. Ye . Asymptotic regulation of time-varying uncertain nonlinear systems with unknown control directions. Automatica , 5 , 929 - 935
-
27)
- E.P. Ryan . A universal adaptive stabilizer for a class of nonlinear systems. Syst. Control Lett. , 4 , 209 - 218
-
28)
- J. Du , C. Guo , S. Yu , Y. Zhao . Adaptive autopilot design of time-varying uncertain ships with completely unknown control coefficient. IEEE J. Ocean. Eng. , 2 , 346 - 352
-
29)
- C.C. Lim , M.Y. Li . Observability analysis of two closed-loop guidance systems with bearings-only measurements. Nonlinear Anal., Real World Appl. , 261 - 286
-
30)
- V.J. Aidala . Kalman filter behavior in bearings-only tracking applications. IEEE Trans. Aerosp. Electron. Syst. , 1 , 29 - 39
-
31)
- F.W. Nesline , P. Zarchan . A new look at classical vs modern homing missile guidance. J. Guid. Control Dyn. , 1 , 78 - 85
-
32)
- D. Zhou , C. Mu , W. Xu . Adaptive sliding-mode guidance of a homing missile. J. Guid. Control Dyn. , 4 , 589 - 594
-
33)
- Y.C. Chang . Intelligent robust control for uncertain nonlinear time-varying systems and its application to robotic. IEEE Trans. Syst. Man Cybern. B, Cybern. , 6 , 1108 - 1119
-
1)