Homing Guidance Law for Cooperative Attack of Multiple Missiles

By In-Soo Jeon, Jin-Ik Lee, Min-Jae Tahk. 2010

586 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Statistical and Nonlinear Physics

View Paper: https://www.semanticscholar.org/paper/3b537e066f7ae56548fe1a5d679f76e56ef0d4a6

How researchers see this paper

The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.

In Aerospace Engineering

1. Vijay R. Kumar
2. Shaojie Shen
3. Dongsoo Cho
4. H. Jin Kim
5. Soon-Jo Chung
6. Philip M. Dames
7. Aditya A. Paranjape
8. Min-Jae Tahk

In Statistical and Nonlinear Physics

1. Dongsoo Cho
2. H. Jin Kim
3. Min-Jae Tahk
4. Debasish Ghose

Citations in the corpus

• Nonsingular Sliding Mode Guidance for Impact Time Control (2016, methodology): “Unlike the guidance laws in [9–13] mentioned previously, which are derived based on linearized engagement dynamics under the small angle assumption of the missile’s flight-path angle, there are other guidance laws related to ITCG based on sliding mode control.”
• A Survey on Aerial Swarm Robotics (2018, background): “Information sharing between the missiles can also be used to directly tune their navigation law, as demonstrated in [107], to achieve a synchronized hit on the target.”