Konstruksi Model Matematika Paralayang dengan Target Pendaratan

Firdo Alhamda Pranata, Hariyanto Hariyanto, Iis Herisman
Submission Date: 2018-11-22 11:49:12
Accepted Date: 2019-05-31 00:00:00

Abstract


Konstruksi model matematika dari pergerakan penerjun dibagi dalam dua pengamatan, yaitu ketika penerjun belum membuka parasut dan setelah penerjun membuka parasut. Pengontrolan dalam penelitian ini dikhususkan saat penerjun sudah membuka parasut hingga mendarat. Untuk mengendalikan parasut, dapat dilakukan dengan cara menggerakkan tali kemudi yang berpusat dibelakang parasut. Dengan menarik tali kemudi kanan ke bawah, maka parasut bergerak ke kanan. Dan jika menarik tali kemudi kiri ke bawah, maka parasut bergerak ke kiri. Untuk mendapatkan model dari paralayang, digunakan metode derivatif dari penurunan Hukum Newton. Dari model yang didapatkan kemudian dikontrol dengan menggunakan PID controller agar penerjun mampu mendarat pada target pendaratan yang diharapkan dengan mengikuti dari setpoint atau lintasan yang telah dibuat sebelumnya

Keywords


Parasut; PID; Pendaratan

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