Impact-time-control guidance law for anti-ship missiles

By In-Soo Jeon, Jin-Ik Lee, Min-Jae Tahk. IEEE Transactions on Control Systems Technology, 2006

645 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Statistical and Nonlinear Physics

View Paper: https://www.semanticscholar.org/paper/0433385f183c4b3adc3f48d3edbdb23e598f7f3b

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. Min-Jae Tahk
2. Dongsoo Cho
3. H. Jin Kim
4. In-Soo Jeon
5. Jin-Ik Lee
6. N. Harl
7. Sivasubramanya Nadar Balakrishnan
8. Radhakant Padhi

In Statistical and Nonlinear Physics

1. Min-Jae Tahk
2. Dongsoo Cho
3. H. Jin Kim
4. In-Soo Jeon
5. Jin-Ik Lee
6. Radhakant Padhi
7. Harshal B. Oza
8. Debasish Ghose

Citations in the corpus

• Homing Guidance Law for Cooperative Attack of Multiple Missiles (2010, methodology): “Here, a cooperative attack means that multiple missiles attack a single target or multiple targets cooperatively or, in a specific case, simultaneously [5,6].”
• 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.”
• Impact Time and Angle Guidance With Sliding Mode Control (2009, background): “Also, since typical CIWS systems can only cover a fanshaped zone which is limited in range and azimuth, controlling the missile impact angles can be another effective means of destroying the target.”