The Development Of a Test Software Suite For Flight Control Laws Evaluation of the LSA-02 UAV Technology Demonstrator

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THE DEVELOPMENT OF A TEST SOFTWARE SUITE FOR FLIGHT CONTROL LAWS EVALUATION OF THE LSA-02 UAV TECHNOLOGY DEMONSTRATOR By TEUKU MORD ICHWANUL HAKIM NIM: 23615015 Aerospace Engineering
Flight Control Laws (FCL) for Basic Electronic Flight Control System (BEFCS) of LSA-02 UAV technology demonstrator has been developed. The FCL has full authority to control the aircraft in all axes. The FCL needs to be evaluated before it is implemented into the aircraft. The evaluation of the FCL is very stringent process. Safety and performance requirements shall be met in any flight condition. Evaluation tool and method shall be developed to allow testing of the FCL in a wide range of flight envelope for both normal and under disturbed conditions. In this thesis a comprehensive concept for FCL verification tool has been developed. The essential part of the concept which are required for an initial FCL verification process has been developed. The implemented characteristic of the software includes the flexibility of the simulation environment to accommodate various FCL and Flight Mechanical Model (FMM) versions. The FCL and FMM are implemented as s-functions in MatlabĀ®/Simulinle environment, to allow automatic execution and freely configurable test, initial condition, operator command, and disturbance input.
To demonstrate the capability of the test software suite, four test cases have been prospected, but only one example test case has been defined in detail. Test case 1000 which evaluate the FCL to a vertical command is defined.
Informasi Detil
Judul Seri -
No. Panggil 50/2019/THE
Penerbit Institut Teknologi Bandung : Bandung.,
Deskripsi Fisik Xvi, 106 hlm.
Bahasa Indonesia
ISBN/ISSN -
Klasifikasi NONE
Edisi 2018
Subyek UAV
LSA-02
Test Software Suite
Pernyataan Tanggungjawab
-
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