Attitude Autopilot for a Gliding Spinning Projectile via Modified Trajectory Linearization Control

Yuchen Wang; Shiyao Lin; Zhichen Yu; Yichen Cheng; Wei Wang

doi:10.1007/978-981-99-9021-4_16

Attitude Autopilot for a Gliding Spinning Projectile via Modified Trajectory Linearization Control

Yuchen Wang^*, Shiyao Lin, Zhichen Yu, Yichen Cheng, Wei Wang

^*Corresponding author for this work

School of Aerospace Engineering

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

Abstract

In this paper, the rapid attitude stabilization problem of guided spinning projectile (GSP) with uncertainties and disturbance is investigated. First, a coupled attitude dynamics model for GSP was developed as control plant with parameter uncertainties and external disturbance. Then a sliding mode based fixed-time trajectory linearization control method is presented with a novel fast fixed-time integral sliding mode (ISM). The ISM is singular-free and ensuring the settling time independent to the initial condition. Moreover, an adaptive sliding mode control (SMC) technique is then synthesized to alleviate SMC inherent chattering. The stability and fixed-time convergence of GSP states are rigorously proved. The numerical simulations are carried out to validate the efficient of proposed control scheme in attenuating system uncertainties.

Original language	English
Title of host publication	Proceedings of 2023 11th China Conference on Command and Control
Publisher	Springer Science and Business Media Deutschland GmbH
Pages	158-170
Number of pages	13
ISBN (Print)	9789819990207
DOIs	https://doi.org/10.1007/978-981-99-9021-4_16
Publication status	Published - 2024
Event	11th China Conference on Command and Control, C2 2023 - Beijing, China Duration: 24 Oct 2023 → 25 Oct 2023

Publication series

Name	Lecture Notes in Electrical Engineering
Volume	1124 LNEE
ISSN (Print)	1876-1100
ISSN (Electronic)	1876-1119

Conference

Conference	11th China Conference on Command and Control, C2 2023
Country/Territory	China
City	Beijing
Period	24/10/23 → 25/10/23

Keywords

Adaptive sliding mode
Fixed-time stable theory
Guided spinning projectile
Integral sliding mode
Trajectory linearization control

Access to Document

10.1007/978-981-99-9021-4_16

Cite this

Wang, Y., Lin, S., Yu, Z., Cheng, Y., & Wang, W. (2024). Attitude Autopilot for a Gliding Spinning Projectile via Modified Trajectory Linearization Control. In Proceedings of 2023 11th China Conference on Command and Control (pp. 158-170). (Lecture Notes in Electrical Engineering; Vol. 1124 LNEE). Springer Science and Business Media Deutschland GmbH. https://doi.org/10.1007/978-981-99-9021-4_16

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title = "Attitude Autopilot for a Gliding Spinning Projectile via Modified Trajectory Linearization Control",

abstract = "In this paper, the rapid attitude stabilization problem of guided spinning projectile (GSP) with uncertainties and disturbance is investigated. First, a coupled attitude dynamics model for GSP was developed as control plant with parameter uncertainties and external disturbance. Then a sliding mode based fixed-time trajectory linearization control method is presented with a novel fast fixed-time integral sliding mode (ISM). The ISM is singular-free and ensuring the settling time independent to the initial condition. Moreover, an adaptive sliding mode control (SMC) technique is then synthesized to alleviate SMC inherent chattering. The stability and fixed-time convergence of GSP states are rigorously proved. The numerical simulations are carried out to validate the efficient of proposed control scheme in attenuating system uncertainties.",

keywords = "Adaptive sliding mode, Fixed-time stable theory, Guided spinning projectile, Integral sliding mode, Trajectory linearization control",

author = "Yuchen Wang and Shiyao Lin and Zhichen Yu and Yichen Cheng and Wei Wang",

note = "Publisher Copyright: {\textcopyright} Chinese Institute of Command and Control 2024.; 11th China Conference on Command and Control, C2 2023 ; Conference date: 24-10-2023 Through 25-10-2023",

year = "2024",

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Wang, Y, Lin, S, Yu, Z, Cheng, Y & Wang, W 2024, Attitude Autopilot for a Gliding Spinning Projectile via Modified Trajectory Linearization Control. in Proceedings of 2023 11th China Conference on Command and Control. Lecture Notes in Electrical Engineering, vol. 1124 LNEE, Springer Science and Business Media Deutschland GmbH, pp. 158-170, 11th China Conference on Command and Control, C2 2023, Beijing, China, 24/10/23. https://doi.org/10.1007/978-981-99-9021-4_16

Attitude Autopilot for a Gliding Spinning Projectile via Modified Trajectory Linearization Control. / Wang, Yuchen; Lin, Shiyao; Yu, Zhichen et al.
Proceedings of 2023 11th China Conference on Command and Control. Springer Science and Business Media Deutschland GmbH, 2024. p. 158-170 (Lecture Notes in Electrical Engineering; Vol. 1124 LNEE).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

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AU - Wang, Yuchen

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N1 - Publisher Copyright: © Chinese Institute of Command and Control 2024.

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