One Engine Out Take-off Trajectory Optimization

Aircraft Maximum TOW (Takeo Weight) is calculated on the SID (Standard Instrument Departure) in the case of a engine failure, so as to respect regulatory constraints. In case of mountainous landscape, a alternative trajectory can be design to reduce obstacle clearance constraints. This trajectory, called EOSID (Engine Out Standard Instrument Departure) is only used in the case of engine failure. Nowadays, EOSID are designed manually by engineers. The aim of this study is to develop a software able to optimize EOSID lateral path so as to maximize the regulatory TOW. In case of mountainous landscape, a alternative takeo trajectory, called EOSID (Engine Out Standard Instrument Departure), can be design to reduce obstacle clearance constraints. The aim of this study is to develop a software able to optimize EOSID lateral path so as to maximize the TOW. In case of mountainous landscape and one engine failure during takeo, an alternative trajectory called EOSID (Engine Out Standard Instrument Departure) that reduces obstacle clearance constraints is flown. This study aims at developing a software that optimizes EOSID lateral path so as to maximize the TOW.