Time‐Varying Sliding Mode Based Fixed‐Time Missile Guidance and Attitude Control With Impact Angle Constraints
Year: 2024
Type: article
DOI: 10.1002/rnc.7694
Authors: Shenghui Wei, Shenmin Song
Institution: Harbin Institute of Technology
Language: English
Topic: Guidance and Control Systems
Subfield: Aerospace Engineering
Field: Engineering
Domain: Physical Sciences
Open Access status: closed
OpenAlex ID: W4404128379