V37 操纵系统及其附件 标准查询与下载
共找到 240 条与 操纵系统及其附件 相关的标准，共 16 页
General requirements for unmanned airship flight control systems
- ICS
- 49.060
- CCS
- V37
- 发布
- 2023-09-07
- 实施
- 2024-01-01
Flight test requirements for flight performance of civil large and medium-sized unmanned helicopter systems
- ICS
- 49.020
- CCS
- V37
- 发布
- 2023-08-06
- 实施
- 2024-03-01
General requirements for the flight control system of civil large and medium-sized unmanned helicopters
- ICS
- 49.020
- CCS
- V37
- 发布
- 2023-08-06
- 实施
- 2024-03-01
本标准规定了民用轻小型固定豆无人机(以下简称"无人机”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无人机飞行控制系统及其部件的设计与验证,其他无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
- ICS
- 49.090
- CCS
- V37
- 发布
- 2020-07-21
- 实施
- 2021-02-01 00:00:00.0
本标准规定了轻小型多旋翼无人机（以下简称 “无人机 ”）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无人机（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。 其他无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
- ICS
- 49.090
- CCS
- V37
- 发布
- 2020-07-21
- 实施
- 2021-02-01 00:00:00.0
本标准规定了民用轻小型无人直升机飞行控制系统的通用要求、验证试验、标识、包装、运输和储存。 本标准适用于民用轻小型无人直升机（起飞重量在 0.25kg～150kg 之间 ）飞行控制系统及其部件的设计与验证。 其他无人驾驶航空器飞行控制系统可参照执行。
General requirements for flight control systems of civil small and light unmanned helicopter
- ICS
- 49.090
- CCS
- V37
- 发布
- 2020-07-21
- 实施
- 2021-02-01 00:00:00.0
Space systems - Space debris mitigation design and operation manual for launch vehicle orbital stages
- ICS
- 49.140
- CCS
- V37
- 发布
- 2021-04-00
- 实施
Small craft. Hydraulic steering systems
- ICS
- 47.020.70;47.080
- CCS
- V37
- 发布
- 2017-12-13
- 实施
- 2017-12-13
Space systems. Programme management. Management of product characteristics
- ICS
- 49.140
- CCS
- V37
- 发布
- 2017-03-31
- 实施
- 2017-03-31
Space systems - Debris mitigation design and operation manual for launch vehicle orbital stages
- ICS
- 49.140
- CCS
- V37
- 发布
- 2017-02-01
- 实施
Space product assurance - Storage, handling and transportation of spacecraft hardware; English version EN 16602-20-08:2016
- ICS
- 49.140
- CCS
- V37
- 发布
- 2016-12
- 实施
Space systems. Space environment (natural and artificial). Observed proton fluences over long duration at GEO and guidelines for selection of confidence level in statistical model of solar proton fluences
- ICS
- 49.140
- CCS
- V37
- 发布
- 2015-12-31
- 实施
- 2015-12-31
Space systems - Interface control documents between ground systems, ground support equipment and launch vehicle with payload
- ICS
- 49.140
- CCS
- V37
- 发布
- 2015-10-15
- 实施
Space systems - Space environment (natural and artificial) - Observed proton fluences over long duration at GEO and guidelines for selection of confidence level in statistical model of solar proton fluences
- ICS
- 49.140
- CCS
- V37
- 发布
- 2015-10
- 实施
本标准规定了民用飞机飞行控制系统(以下简称飞行控制系统)模拟器试验、地面综合试验和机上地面试验等地面试验的要求。 本标准适用于民用飞机飞行控制系统的地面试验。
Ground test requirements for flight control system of civil aircraft
- ICS
- 49.090
- CCS
- V37
- 发布
- 2014-05-19
- 实施
- 2014-10-01
本标准规定了民用飞机飞行控制系统(以下简称飞行控制系统)的安全性设计、适航性设计、可靠性设计、维修性设计、系统安装和主飞行控制系统设计、辅助飞行控制系统设计、自动飞行控制系统设计等设计和安装要求。 本标准适用于民用飞机飞行控制系统的研制。
Design and installation requirements for flight control system of civil aircraft
- ICS
- 49.090
- CCS
- V37
- 发布
- 2014-05-19
- 实施
- 2014-10-01
本标准规定了民用飞机飞行控制系统飞行试验的内容和要求。 本标准适用于民用运输类飞机电传飞行控制系统的飞行试验。其他类飞机可参照使用。
Requirements for flight test of civil aircraft flight control system
- ICS
- 49.020
- CCS
- V37
- 发布
- 2014-05-19
- 实施
- 2014-10-01
本标准规定了民用飞机飞行控制系统(以下简称飞行控制系统)的尺寸、重量、材料、性能、环境适应性、电磁兼容性、安全性、可靠性、维修性、测试性、互换性等技术要求以及相应的验证要求。 本标准适用于民用飞机飞行控制系统的研制。
General requirements for flight control system of civil aircraft
- ICS
- 49.090
- CCS
- V37
- 发布
- 2014-05-19
- 实施
- 2014-10-01
(a) Definitions. For purpose of this section
Aeronautics and Space. Part121:Operating requirements. Section121.579:Minimum altitudes for use of autopilot.
- ICS
- CCS
- V37
- 发布
- 2014-02-03
- 实施
- 2014-02-03
The purpose of this document is to develop the general characteristics and requirements for feel-force control systems for active cockpit controllers, also known as Active Inceptors. The document presents technical material that describes the recommended key characteristics and design considerations for these types of systems. Where appropriate, the effects of platform specific requirements (e.g., single axis/dual axis, single seat/dual seat, civil/military, rotorcraft/fixed wing aircraft, etc.) are clearly identified. The material developed will serve as a reference guide for: a. Aircraft prime contractors who want to understand active cockpit controller t
Aerospace Active Inceptor Systems for Aircraft Flight and Engine Controls
- ICS
- 49.090
- CCS
- V37
- 发布
- 2013-02-11
- 实施
