نتناولُ في هذه الأطروحةِ مسألة اَلهبوطِ الاضطراريِّ لطائرةٍ غيرِ مأهولةٍ ثابتةِ الجناحِ فاقدةٍ للدفعِ على أرضٍمستو يةٍ أو متسلقةٍ محدودةِ الأبعاد. نركز فُي بحثنا على الطائراتِ متوسطةِ الحجمِ التي ٺتطلبُ القيامَ بهبوطٍ تقليديٍّ على عجلات، بينما تقتصر سُطوحُ التحكمِ المتوفرة فُيها على السطوحِ الرئيسيةِ فقط، أي دفةِ الارتفاعِ و دفةِ التوجيهِ و الجنيحات، دونَ أيِّ سطوحٍ مخصصةٍ للتحكمِ بالكبح.
This research tackles autolanding a power-off fixed-wing Unmanned Aerial Vehicle (UAV) on a
level or uphill landing strip with limited dimensions. New approaches to path planning, guidance,
and control are proposed for the final approach and landing stages. These approaches address
mid-sized UAVs assuming that the aircraft has only standard control surfaces, i.e. the elevator,
the rudder, and the ailerons. This problem has not been covered by the existing flight control
literature.
References used
Douglas M Marshall, Richard K Barnhart, Eric Shappee, and Michael Thomas Most. Introduction to unmanned aircraft systems. Crc Press, 2015
Reg Austin. Unmanned aircraft systems: UAVs design, development and deployment, volume 54. John Wiley & Sons, 2011
Paul Fahlstrom and Thomas Gleason. Introduction to UAV systems. John Wiley & Sons, 2012
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