Optimal Guidance Law Based on Virtual Sliding Target-Reference-Cited by-同舟云学术

Optimal Guidance Law Based on Virtual Sliding Target

Published:2017-05 Issue:3 Volume:30 Page:04016097
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Mozaffari Mohiyeddin¹,Safarinejadian Behrouz²,Binazadeh Tahereh³

Affiliation:

1. Ph.D. Student, Dept. of Electrical Engineering, Shiraz Univ. of Technology, Shiraz, 71555313 Fars, Iran.

2. Associated Professor, Dept. of Electrical Engineering, Shiraz Univ. of Technology, Shiraz, 71555313 Fars, Iran (corresponding author).

3. Assistant Professor, Dept. of Electrical Engineering, Shiraz Univ. of Technology, Shiraz, 71555313 Fars, Iran.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0000692

Reference29 articles.

1. Proportional Guidance and CDM Control Synthesis for a Short-Range Homing Surface-to-Air Missile

2. Chen J. Tian Y. Liu H. H. and Ren Z. (2010). “Autopilot design for a side-jet missile based on MRVSS technique and GA optimization.” Earth and Space: Proc. 12th Int. Conf. on Engineering Science Construction and Operations in Challenging Environments 1821–1833.

3. Modified Pure Proportional Navigation Guidance Law for Impact Time Control

4. Proportional Navigation With Delayed Line-of-Sight Rate

5. 3D guidance law modeling

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