Work

Trajectory Control of Midcourse Guidance for Air-to-Air Missile Based on Feedback Linearization and Sliding Mode Control

Year: 2024

Type: conference-paper

Source: IEEE International Conference on Unmanned Systems (ICUS)

DOI: 10.1109/icus61736.2024.10840132

Authors: Chencheng Zhang, Zhiqiang Tong, Hongquan Liu, Weijian Pang

Institution: Nanjing University of Aeronautics and Astronautics

Language: English

Topic: Guidance and Control Systems

Subfield: Aerospace Engineering

Field: Engineering

Domain: Physical Sciences

Open Access status: closed

Funder: National Natural Science Foundation of China

Award: G678760520

OpenAlex ID: W4406728723

FWCI:

Cites: 27

Cited by:

Related to: 10