NDLI: Finite-time sliding mode guidance law design with impact angle constraints

Content Provider	IEEE Xplore Digital Library
Author	Zhou Hui-bo Liu Hong-liang Song Shen-min
Copyright Year	2014
Description	Author affiliation: Sch. of Math. Sci., Harbin Normal Univ., Harbin, China (Liu Hong-liang) \|\| Center for Control Theor. & Guidance Technol., Harbin Inst. of Technol., Harbin, China (Zhou Hui-bo; Song Shen-min)
Abstract	For the missile-target relative motion equations in the two-dimensional plane, a sliding mode guidance law design problem with terminal line-of-sight angle constraints in maneuvering target intercept is investigated in this paper. The attack angle constraints are transformed into line-of-sight angle constraints. A finite-time convergent linear sliding mode surface including the desired line-of-sight angle and the line-of-sight angle rate is selected. According to the target maneuvering in the system of a first-order sliding mode, the total perturbations of the target is estimated in finite time by using a non-homogeneous disturbance observer. Then guidance law is designed by using a fast power reaching law with a second-order sliding mode characteristics. Simulation results show that the missile can intercept the target with high accuracy within the desired line-of-sight angle. Meanwhile the disturbance observer can achieve the fast and high-precision estimation of the total target disturbances.
Starting Page	675
Ending Page	680
File Size	190457
Page Count	6
File Format	PDF
ISBN	9789881563873
ISSN	19341768
DOI	10.1109/ChiCC.2014.6896706
Language	English
Publisher	Institute of Electrical and Electronics Engineers, Inc. (IEEE)
Publisher Date	2014-07-28
Publisher Place	China
Access Restriction	Subscribed
Rights Holder	TCCT, CAA
Subject Keyword	Missiles Navigation Simulation Sliding mode Observer Observers Acceleration Transient analysis Impact angle Equations Guidance law Finite time
Content Type	Text
Resource Type	Article

Sl.	Authority	Responsibilities	Communication Details
1	Ministry of Education (GoI), Department of Higher Education	Sanctioning Authority	https://www.education.gov.in/ict-initiatives
2	Indian Institute of Technology Kharagpur	Host Institute of the Project: The host institute of the project is responsible for providing infrastructure support and hosting the project	https://www.iitkgp.ac.in
3	National Digital Library of India Office, Indian Institute of Technology Kharagpur	The administrative and infrastructural headquarters of the project	Dr. B. Sutradhar bsutra@ndl.gov.in
4	Project PI / Joint PI	Principal Investigator and Joint Principal Investigators of the project	Dr. B. Sutradhar bsutra@ndl.gov.in Prof. Saswat Chakrabarti will be added soon
5	Website/Portal (Helpdesk)	Queries regarding NDLI and its services	support@ndl.gov.in
6	Contents and Copyright Issues	Queries related to content curation and copyright issues	content@ndl.gov.in
7	National Digital Library of India Club (NDLI Club)	Queries related to NDLI Club formation, support, user awareness program, seminar/symposium, collaboration, social media, promotion, and outreach	clubsupport@ndl.gov.in
8	Digital Preservation Centre (DPC)	Assistance with digitizing and archiving copyright-free printed books	dpc@ndl.gov.in
9	IDR Setup or Support	Queries related to establishment and support of Institutional Digital Repository (IDR) and IDR workshops	idr@ndl.gov.in

Design of guidance law based on nonsingular terminal sliding mode control and finite-time disturbance observer*

Design of terminal sliding-mode guidance law with attack angle constraints

An observer-based missile guidance law

Finite time convergent sliding-mode guidance law with impact angle constraint

Three-dimensional guidance law design with impact time constraint

Optimal sliding mode guidance law with height deviation and terminal impact angle constraints

A continuous second-order sliding mode guidance against highly maneuverable targets

Guidance law accounting for second-order dynamics of missile autopilot and impact angle constraints

Adaptive sliding-mode guidance law with finite time convergence

Finite-time sliding mode guidance law design with impact angle constraints

Similar Documents

Design of guidance law based on nonsingular terminal sliding mode control and finite-time disturbance observer*

Design of terminal sliding-mode guidance law with attack angle constraints

An observer-based missile guidance law

Finite time convergent sliding-mode guidance law with impact angle constraint

Three-dimensional guidance law design with impact time constraint

Optimal sliding mode guidance law with height deviation and terminal impact angle constraints

A continuous second-order sliding mode guidance against highly maneuverable targets

Guidance law accounting for second-order dynamics of missile autopilot and impact angle constraints

Adaptive sliding-mode guidance law with finite time convergence

Finite-time sliding mode guidance law design with impact angle constraints