A Terminal Guidance Law Based on Motion Camouflage Strategy of Air-to-Ground Missiles

3Citations
Citations of this article
15Readers
Mendeley users who have this article in their library.

Abstract

A guidance law for attacking ground target based on motion camouflage strategy is proposed in this paper. According to the relative position between missile and target, the dual second-order dynamics model is derived. The missile guidance condition is given by analyzing the characteristic of motion camouflage strategy. Then, the terminal guidance law is derived by using the relative motion of missile and target and the guidance condition. In the process of derivation, the three-dimensional guidance law could be designed in a two-dimensional plane and the difficulty of guidance law design is reduced. A two-dimensional guidance law for three-dimensional space is derived by bringing the estimation for target maneuver. Finally, simulation for the proposed guidance law is taken and compared with pure proportional navigation. The simulation results demonstrate that the proposed guidance law can be applied to air-to-ground missiles.

References Powered by Scopus

Optimal guidance laws with terminal impact angle constraint

578Citations
N/AReaders
Get full text

Biased PNG law for impact with angular constraint

557Citations
N/AReaders
Get full text

Impact time and angle guidance with sliding mode control

421Citations
N/AReaders
Get full text

Cited by Powered by Scopus

Camouflage in a dynamic world

44Citations
N/AReaders
Get full text

Optimal Maneuver Trajectory for Hypersonic Missiles in Dive Phase Using Inverted Flight

12Citations
N/AReaders
Get full text

Adaptive terminal guidance law with impact-angle constraint

7Citations
N/AReaders
Get full text

Register to see more suggestions

Mendeley helps you to discover research relevant for your work.

Already have an account?

Cite

CITATION STYLE

APA

Gao, C. S., Li, J. Q., & Jing, W. X. (2016). A Terminal Guidance Law Based on Motion Camouflage Strategy of Air-to-Ground Missiles. International Journal of Aerospace Engineering, 2016. https://doi.org/10.1155/2016/9218754

Readers over time

‘17‘18‘19‘21‘22‘23‘2402468

Readers' Seniority

Tooltip

PhD / Post grad / Masters / Doc 2

67%

Researcher 1

33%

Readers' Discipline

Tooltip

Psychology 2

40%

Agricultural and Biological Sciences 1

20%

Computer Science 1

20%

Engineering 1

20%

Save time finding and organizing research with Mendeley

Sign up for free
0