The DOI matches its Crossref record; 25 of the 25 references it cites were found in a registry or an index.
Back-stepping active disturbance rejection control design for integrated missile guidance and control system via reduced-order ESO
Abstract
This paper proposes a novel composite integrated guidance and control (IGC) law for missile intercepting against unknown maneuvering target with multiple uncertainties and control constraint. First, by using back-stepping technique, the proposed IGC law design is separated into guidance loop and control loop. The unknown target maneuvers and variations of aerodynamics parameters in guidance and control loop are viewed as uncertainties, which are estimated and compensated by designed model-assisted reduced-order extended state observer (ESO). Second, based on the principle of active disturbance rejection control (ADRC), enhanced feedback linearization (FL) based control law is implemented for the IGC model using the estimates generated by reduced-order ESO. In addition, performance analysis and comparisons between ESO and reduced-order ESO are examined. Nonlinear tracking differentiator is employed to construct the derivative of virtual control command in the control loop. Third, the closed-loop stability for the considered system is established. Finally, the effectiveness of the proposed IGC law in enhanced interception performance such as smooth interception course, improved robustness against multiple uncertainties as well as reduced control consumption during initial phase are demonstrated through simulations.
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“Although increasing the ESO gains may improve the estimation accuracy, it would also amplify noises, leading to the so-called peaking phenomenon [45,46], or even system instability.”
From Compensation Function Observer-Based Backstepping Sliding-Mode Control of Uncertain Electro-Hydraulic Servo System (2024) · cites this paper as [45]
Citations
Cites
From PID to Active Disturbance Rejection Control
Han, J. (2009) · IEEE Transactions on Industrial Electronics · doi:10.1109/tie.2008.2011621 · Cited by 6,803
Scaling and bandwidth-parameterization based controller tuning
Gao, Z. (2005) · Proceedings of the ... American Control Conference/Proceedings of the American Control Conference · doi:10.1109/acc.2003.1242516 · Cited by 2,453
Active disturbance rejection control: Methodology and theoretical analysis
Huang, Y., & Xue, W. (2014) · ISA Transactions · doi:10.1016/j.isatra.2014.03.003 · Cited by 897
Nonsingular Terminal Sliding Mode Guidance with Impact Angle Constraints
Kumar, S. R., Rao, S., & Ghose, D. (2014) · Journal of Guidance Control and Dynamics · doi:10.2514/1.62737 · Cited by 385
Sliding-Mode Guidance and Control for All-Aspect Interceptors with Terminal Angle Constraints
Kumar, S. R., Rao, S., & Ghose, D. (2012) · Journal of Guidance Control and Dynamics · doi:10.2514/1.55242 · Cited by 337
On convergence of tracking differentiator
Guo, B., & Zhao, Z. (2011) · International Journal of Control · doi:10.1080/00207179.2011.569954 · Cited by 287
Integrated Guidance and Control of Missiles With$theta hbox - D$Method
Xin, M., Balakrishnan, S. N., & Ohlmeyer, E. J. (2006) · IEEE Transactions on Control Systems Technology · doi:10.1109/tcst.2006.876903 · Cited by 189
Integrated design of agile missile guidance and autopilot systems
Menon, P. K., & Ohlmeyer, E. J. (2001) · Control Engineering Practice · doi:10.1016/s0967-0661(01)00082-x · Cited by 171
Shao, X., & Wang, H. (2014) · ISA Transactions · doi:10.1016/j.isatra.2014.06.010 · Cited by 155
Missile Guidance Law Based on Extended State Observer
Zhu, Z. H., Xu, D., Liu, J., & Xia, Y. (2012) · IEEE Transactions on Industrial Electronics · doi:10.1109/tie.2012.2232254 · Cited by 151
Flagged first, then by citations
Research works printed but not linked: 2
- Yan, 2013, Adaptive integrated guidance and control based on backstepping and input-to-state stability, Asian J Control, 1
- Dong, 2011, Active disturbance rejection control for an electrostatically actuated MEMS device, J Intel Control Syst, 16, 160
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Sorted by citations
Nonsingular Terminal Sliding Mode Guidance with Impact Angle Constraints
Kumar, S. R., Rao, S., & Ghose, D. (2014) · Journal of Guidance Control and Dynamics · doi:10.2514/1.62737 · Cited by 385
Liu, L., Wang, D., & Peng, Z. (2016) · IEEE Journal of Oceanic Engineering · doi:10.1109/joe.2016.2569218 · Cited by 376
“Second, since the order of the proposed ESO is identical to one, the peaking performance during the transient state can be substantially eliminated [18].”
BackgroundInfluentialA Novel Fuzzy Observer-Based Steering Control Approach for Path Tracking in Autonomous Vehicles
Zhang, C., Hu, J., Qiu, J., Yang, W., Sun, H., & Chen, Q. (2018) · IEEE Transactions on Fuzzy Systems · doi:10.1109/tfuzz.2018.2856187 · Cited by 183
Shao, X., Liu, J., & Wang, H. (2017) · Mechanical Systems and Signal Processing · doi:10.1016/j.ymssp.2017.11.034 · Cited by 141
Huang, Z., Li, Y., Liu, Y., Sui, W., & Zhang, G. (2018) · Mathematical Problems in Engineering · doi:10.1155/2018/3905879 · Cited by 133
“For example, in 2015, Shao thought that the ADRC was available to a cascaded integral system, such as a motion control system [10].”
Metadata
- Authors
- Xingling, S., & Honglun, W.
- Affiliations
- Beihang University (CN)
- Corresponding author
- Honglun, Wang
- Venue
- ISA Transactions
- Publisher
- Elsevier BV
- Published
- 2015-07
- Volume
- 57
- Pages
- 10-22
- ISSN
- 0019-0578 (ISSN-L)
- OpenAlex
- W2008500509
- Cited by
- 196
- References
- 25
- Citations by year
- 2026: 8 · 2025: 10 · 2024: 20 · 2023: 20 · 2022: 16 · 2021: 14 · 2020: 19 · 2019: 27 · 2018: 25 · 2017: 21 · 2016: 13 · 2015: 2
- FWCI
- 29.52
- Type
- journal article
- Language
- en
- Open access
- closed
- Locations
- ISA Transactions (publishedVersion)
- PubMed (publishedVersion)
- Funders
- National Natural Science Foundation of China (61175084/F030601)
- Program for Changjiang Scholars and Innovative Research Team in University (IRT 13004)
- Aeronautical Science Foundation of China (2014ZA51002)
- Topics
- Physical Sciences › Engineering › Aerospace Engineering › Guidance and Control Systems
- Physical Sciences › Engineering › Control and Systems Engineering › Adaptive Control of Nonlinear Systems
- Physical Sciences › Engineering › Aerospace Engineering › Aerospace Engineering and Control Systems
- Keywords
- integrated guidance and control, missile intercept, backstepping control, active disturbance rejection control, reduced-order extended state observer, feedback linearization, nonlinear tracking differentiator, input constraints, robustness to uncertainty, closed-loop stability
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