NDLI: A guidance law with impact angle constraint for anti-ship missiles cooperative attack

Content Provider	IEEE Xplore Digital Library
Author	Wu Xiaolong Wu Sentang Xing Zhihui
Copyright Year	2014
Description	Author affiliation: Sch. of Autom. Sci. & Electr. Eng., Beijing Univ. of Aeronaut. & Astronaut., Beijing, China (Wu Xiaolong; Wu Sentang; Xing Zhihui)
Abstract	Based on the kinematics and dynamics of missile-to-target relative motion and the method of time-to-go estimation, a biased proportional guidance (BPG) law that can reduce the impact time variance is designed and proved. Then a time cooperative guidance law with impact angle constraint for two missile formations is designed, based on the guidance law with terminal angle constraint. The impact angle is controlled by the hand-over area position, and flight path angle in the hand-over area is constrained considering the overload limitation. The missile is guided to the designed hand-over area with a certain path angle and arrival time cooperative control. In the terminal guidance, the missile is guided by the time cooperative guidance law and the two formations are planned with converging at the mutually perpendicular direction, to reduce the influence of the target maneuver and jamming. Finally, the convergence of time-to-go variance under the influence of communication update rate is presented, and six degrees of freedom (6-DOF) simulation results are given. Simulations demonstrate that the proposed designs can satisfy the requirements of impact time deviation and angle as well as the guidance precision.
Starting Page	954
Ending Page	959
File Size	177638
Page Count	6
File Format	PDF
ISBN	9789881563873
ISSN	19341768
DOI	10.1109/ChiCC.2014.6896756
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 Simulation Cooperative Attack Estimation Time Cooperation Handover Impact Angle Anti-ship missile Guidance Law Trajectory Convergence
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 Anti-Ship Missile's Terminal Guidance Law with Multiple Constraint Based on Backstepping

Improvement of guidance law for simultaneous attack

Design of variable structure guidance law with constraints on impact angle for anti-ship missile

Cooperative guidance law with time constraint for multiple missiles

Fixed-Time Cooperative Guidance Law With Angle Constraint for Multiple Missiles Against Maneuvering Target

Distributed multi-missile salvo attack

Guidance law with finite time convergence subject to impact angle constraint

Time-to-go estimation filter for anti-ship missile application

Research of guidance law of missile with terminal angular constraint

A guidance law with impact angle constraint for anti-ship missiles cooperative attack

Similar Documents

Design of Anti-Ship Missile's Terminal Guidance Law with Multiple Constraint Based on Backstepping

Improvement of guidance law for simultaneous attack

Design of variable structure guidance law with constraints on impact angle for anti-ship missile

Cooperative guidance law with time constraint for multiple missiles

Fixed-Time Cooperative Guidance Law With Angle Constraint for Multiple Missiles Against Maneuvering Target

Distributed multi-missile salvo attack

Guidance law with finite time convergence subject to impact angle constraint

Time-to-go estimation filter for anti-ship missile application

Research of guidance law of missile with terminal angular constraint

A guidance law with impact angle constraint for anti-ship missiles cooperative attack