Abstract

Wave-off judgment research of carrier-borne aircraft in the landing process led by automatic landing system is made and the conception of security window in automatic Landing of the carrier-borne aircraft is proposed. Through the study of carrier-borne aircraft’s automatic safety window landing position, and calculates the boundary of safety window.

Highlights

  • The landing of carrier-borne aircraft is different from that of land-based aircraft

  • When the aircraft goes through safety window 15 sec far from the stern in automatic landing and if it cannot land within the ideal landing range under the guidance of ACLS, so at this time retrial flight should be in operation

  • Aircraft carrier air-wake model: Air wake’s effect on carrier-borne aircraft landing is caused by the air flow rate in the stern flow changes, so the air-wake model must be able to reflect the changes of the wind speed in and that of 5 sec, with vertical deviation from -9 to 9 m, in full automatic the path curve under the guidance of landing system

Read more

Summary

INTRODUCTION

GUIDING SYSTEM caused by wave causes changes of the ideal landing point, filtering position changes of the ideal landing. When the aircraft goes through safety window 15 sec far from the stern in automatic landing and if it cannot land within the ideal landing range under the guidance of ACLS, so at this time retrial flight should be in operation. Roll spectrum transfer function: Fig. 6: Different longitudinal deviation path curve of carrier- This fitting method of simplifying carrier motion at sea power spectrum is very intuitive in use, simple. Aircraft carrier air-wake model: Air wake’s effect on carrier-borne aircraft landing is caused by the air flow rate in the stern flow changes, so the air-wake model must be able to reflect the changes of the wind speed in and that of 5 sec, with vertical deviation from -9 to 9 m, in full automatic the path curve under the guidance of landing system. The random carrier air-wake disturbance: Random atmospheric turbulence caused by the existence of aircraft carrier, power measurement of the spectra shows that this part of the atmospheric turbulence is anisotropic

CONCLUSION
Full Text
Paper version not known

Talk to us

Join us for a 30 min session where you can share your feedback and ask us any queries you have

Schedule a call

Disclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.