Autopilot Design for Bank-to-Turn Missiles Using Receding Horizon Predictive Control Scheme
Year: 1997
Type: article
DOI: 10.2514/2.4184
Institutions: Seoul National University, Agency for Defense Development
Language: English
Topic: Guidance and Control Systems
Subfield: Aerospace Engineering
Field: Engineering
Domain: Physical Sciences
Open Access status: closed
OpenAlex ID: W2047613019