发布时间:2024-05-27 17:49:26 - 更新时间:2024年06月29日 15:22
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本标准规定了民用轻小型固定豆人机(以下简称"人机”飞行控制系统的通用要求、验证试验、标识`包装、运输和贮存。本标准适用于最大起飞重量在0.25 kg一150 kg 之间的民用轻小型固定避人机飞行控制系统及其部件的设计与验证,其他人机飞行控制系统可参照执行
General requirements for the flight control system of civil small and light fixed wing unmanned aircraft
本标准规定了轻小型多旋翼人机(以下简称 “人机 ”)飞行控制与导航系统的通用要求、验证试验以及标识、包装、运输和贮存要求。 本标准适用于轻小型多旋翼人机(起飞重量在 0.25kg~150kg 之间 )的飞行控制与导航系统设计与制造。 其他人机飞行控制与导航系统可参照执行
General requirements for the flight control and navigation system of small and light multi-rotor unmanned aircraft
《多旋翼人机飞行控制系统半实物仿真测试方法》,提供了对飞控样品进行功能性能和安全性的半实物仿真测试方法。功能性能半实物仿真测试包括:硬件在环起飞与着陆、硬件在环控制模式切换、硬件在环飞行控制测试、一键返航与自主降落;安全性半实物仿真测试包括:陀螺仪故障注入、加速度计故障注入、磁力计故障注入、电机
Semi-physical simulation test method for the flight control system of multi-rotor unmaned aircraft
《多旋翼人机飞行控制系统半实物仿真测试方法》,提供了对飞控样品进行功能性能和安全性的半实物仿真测试方法。功能性能半实物仿真测试包括:硬件在环起飞与着陆、硬件在环控制模式切换、硬件在环飞行控制测试、一键返航与自主降落;安全性半实物仿真测试包括:陀螺仪故障注入、加速度计故障注入、磁力计故障注入、电机
Semi-physical simulation test method for the flight control system of multi-rotor unmaned aircraft
General Technical Specifications for Overhead Power Line Multi-rotor UAV Flight Control System
Manned aircraft (fixed wing) flight performance
Manned aircraft (fixed wing) flight quality
本标准规定了固定翼人机系统的术语和定义、分类、技术要求、标志、包装、运输和贮存
Technical Requirements for Fixed Wing UAV System
This document specifies the composition, functional and performance requirements of flight controls for civil multicopter unmanned aircrafts (UAs
Flight control system for civil small and light multicopter unmanned aircraft system (UAS) — General requirements
外观要求、拦截性能、发射频率、发射功率、环境适应性要求
UAV interception control system
This document specifies the composition, functional and performance requirements of flight controls for civil multicopter unmanned aircrafts (UAs
Flight control system for civil small and light multicopter unmanned aircraft system (UAS). General requirements (British Standard)
General requirements for unmanned airship flight control systems
BS ISO 24355. General requirements of flight control system for civil small and light multirotor UAS
本标准规定了民用旋翼人机系统飞行环境保障、飞行前飞行器检查、飞行过程中和飞行降落后的操作、电池维护和飞机维护
Flight safety operation specification for civil rotor UAV system
Flight performance of civil light and small multi-rotor unmanned aerial vehicle system
本标准规定了民用轻小型固定豆人机(以下简称"人机”飞行控制系统的通用要求、验证试验、标识`包装、运输和贮存。本标准适用于最大起飞重量在0.25 kg一150 kg 之间的民用轻小型固定避人机飞行控制系统及其部件的设计与验证,其他人机飞行控制系统可参照执行
General requirements for the flight control system of civil small and light fixed wing unmanned aircraft
本标准规定了轻小型多旋翼人机(以下简称 “人机 ”)飞行控制与导航系统的通用要求、验证试验以及标识、包装、运输和贮存要求。 本标准适用于轻小型多旋翼人机(起飞重量在 0.25kg~150kg 之间 )的飞行控制与导航系统设计与制造。 其他人机飞行控制与导航系统可参照执行
General requirements for the flight control and navigation system of small and light multi-rotor unmanned aircraft
《多旋翼人机飞行控制系统半实物仿真测试方法》,提供了对飞控样品进行功能性能和安全性的半实物仿真测试方法。功能性能半实物仿真测试包括:硬件在环起飞与着陆、硬件在环控制模式切换、硬件在环飞行控制测试、一键返航与自主降落;安全性半实物仿真测试包括:陀螺仪故障注入、加速度计故障注入、磁力计故障注入、电机
Semi-physical simulation test method for the flight control system of multi-rotor unmaned aircraft
《多旋翼人机飞行控制系统半实物仿真测试方法》,提供了对飞控样品进行功能性能和安全性的半实物仿真测试方法。功能性能半实物仿真测试包括:硬件在环起飞与着陆、硬件在环控制模式切换、硬件在环飞行控制测试、一键返航与自主降落;安全性半实物仿真测试包括:陀螺仪故障注入、加速度计故障注入、磁力计故障注入、电机
Semi-physical simulation test method for the flight control system of multi-rotor unmaned aircraft
General Technical Specifications for Overhead Power Line Multi-rotor UAV Flight Control System
Manned aircraft (fixed wing) flight quality
Manned aircraft (fixed wing) flight performance
本标准规定了固定翼人机系统的术语和定义、分类、技术要求、标志、包装、运输和贮存
Technical Requirements for Fixed Wing UAV System
This document specifies the composition, functional and performance requirements of flight controls for civil multicopter unmanned aircrafts (UAs
Flight control system for civil small and light multicopter unmanned aircraft system (UAS) — General requirements
外观要求、拦截性能、发射频率、发射功率、环境适应性要求
UAV interception control system
This document specifies the composition, functional and performance requirements of flight controls for civil multicopter unmanned aircrafts (UAs
Flight control system for civil small and light multicopter unmanned aircraft system (UAS). General requirements (British Standard)
General requirements for unmanned airship flight control systems
BS ISO 24355. General requirements of flight control system for civil small and light multirotor UAS
本标准规定了民用旋翼人机系统飞行环境保障、飞行前飞行器检查、飞行过程中和飞行降落后的操作、电池维护和飞机维护
Flight safety operation specification for civil rotor UAV system
Flight performance of civil light and small multi-rotor unmanned aerial vehicle system