Instantaneous Impact Point Guidance Considering Uncertainty in Engine Cutoff Time-Reference-Cited by-同舟云学术

Instantaneous Impact Point Guidance Considering Uncertainty in Engine Cutoff Time

Published:2020-02 Issue:2 Volume:43 Page:373-382
ISSN:1533-3884
Container-title:Journal of Guidance, Control, and Dynamics
language:en
Short-container-title:Journal of Guidance, Control, and Dynamics

Author:

Jo Byeong-Un¹,Ahn Jaemyung¹,Roh Woong-Rae²

Affiliation:

1. Korea Advanced Institute of Science and Technology, Daejeon 34141, Republic of Korea

2. Korea Aerospace Research Institute, Daejeon 34133, Republic of Korea

Funder

National Research Foundation of Korea

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering

Reference10 articles.

1. Near time-optimal feedback instantaneous impact point (IIP) guidance law for rocket

2. Free Flight of a Ballistic Missile

3. ZarchanP., Tactical and Strategic Missile Guidance, 6th ed., Progress in Astronautics and Aeronautics, AIAA, Reston, VA, 2013, pp. 290–298. 10.2514/4.868948

4. Optimal In-Flight Trajectory Modifications for Ballistic Missiles and Free Rockets

5. Guidance and targeting for the strategic target system

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