前言 根据仰卧飞行时+Gz耐力增强这一事实,本工作的目的是为了未来座舱设计评价高性能仰卧飞行的可行性。 方法 在海军空战中心(NAWC)动力飞行模拟器上,改进并部署美国空军(USAF)座舱逃生组件(65°椅背角,SBA)。一个高保真战斗机航模,匹配有由计算机产生的宽带视野显示、平视显示器(HUD)、驾驶杆、油门和方向舵脚镫。7名男性受试者(飞行经验从首次飞行到战斗机飞行员),接受地面训练,以执行 Preface According to the fact that + Gz endurance is increased during supine flight, the purpose of this work is to evaluate the feasibility of a high performance supine flight for future cockpit design. Methods The USAF cockpit escape kit (65 ° seatback, SBA) was retrofitted and deployed at the Navy Air Combat Center (NAWC) powered flight simulator. A high fidelity fighter jet model, matched by a computer-generated broadband field of view display, head-up display (HUD), steering, throttle and rudder 镫. Seven male subjects (flying experience from first flight to fighter pilot) received ground training to perform