Control of a VTOL Aircraft Model with Air-Launched Missile Release Impact and Wind Disturbances

Sivrioglu S., BAŞARAN S.

9th International Conference on Mechanical Engineering and Robotics Research, ICMERR 2025, Barcelona, İspanya, 15 - 17 Ocak 2025, ss.187-191, (Tam Metin Bildiri) identifier

  • Yayın Türü: Bildiri / Tam Metin Bildiri
  • Doi Numarası: 10.1109/icmerr64601.2025.10949912
  • Basıldığı Şehir: Barcelona
  • Basıldığı Ülke: İspanya
  • Sayfa Sayıları: ss.187-191
  • Anahtar Kelimeler: air-launched missile, Trajectory control, unsymmetric structure, VTOL
  • Bilecik Şeyh Edebali Üniversitesi Adresli: Evet

Özet

This study focuses on vertical take-off and landing (VTOL) unmanned aircraft, examining the impact of air-launched missile releases on the system. The release process not only disrupts the system's symmetric structure but also alters its mass and inertia parameters. To address these challenges, the study introduces a model to analyze the effects of missile releases and incorporates a wind turbulence model to evaluate aircraft performance under various scenarios. The study focusses on understanding the impact of missile release on UAV performance, particularly under realistic turbulence conditions that are critical for VTOL operations.