V37 操縱系統(tǒng)及其附件 標(biāo)準(zhǔn)查詢(xún)與下載
共找到 240 條與 操縱系統(tǒng)及其附件 相關(guān)的標(biāo)準(zhǔn)，共 16 頁(yè)
General requirements for unmanned airship flight control systems
- ICS
- 49.060
- CCS
- V37
- 發(fā)布
- 2023-09-07
- 實(shí)施
- 2024-01-01
Flight test requirements for flight performance of civil large and medium-sized unmanned helicopter systems
- ICS
- 49.020
- CCS
- V37
- 發(fā)布
- 2023-08-06
- 實(shí)施
- 2024-03-01
General requirements for the flight control system of civil large and medium-sized unmanned helicopters
- ICS
- 49.020
- CCS
- V37
- 發(fā)布
- 2023-08-06
- 實(shí)施
- 2024-03-01
本標(biāo)準(zhǔn)規(guī)定了民用輕小型固定豆無(wú)人機(jī)(以下簡(jiǎn)稱(chēng)"無(wú)人機(jī)”飛行控制系統(tǒng)的通用要求、驗(yàn)證試驗(yàn)、標(biāo)識(shí)`包裝、運(yùn)輸和貯存。本標(biāo)準(zhǔn)適用于最大起飛重量在0.25 kg一150 kg 之間的民用輕小型固定避無(wú)人機(jī)飛行控制系統(tǒng)及其部件的設(shè)計(jì)與驗(yàn)證,其他無(wú)人機(jī)飛行控制系統(tǒng)可參照?qǐng)?zhí)行
General requirements for the flight control system of civil small and light fixed wing unmanned aircraft
- ICS
- 49.090
- CCS
- V37
- 發(fā)布
- 2020-07-21
- 實(shí)施
- 2021-02-01 00:00:00.0
本標(biāo)準(zhǔn)規(guī)定了輕小型多旋翼無(wú)人機(jī)（以下簡(jiǎn)稱(chēng) “無(wú)人機(jī) ”）飛行控制與導(dǎo)航系統(tǒng)的通用要求、驗(yàn)證試驗(yàn)以及標(biāo)識(shí)、包裝、運(yùn)輸和貯存要求。 本標(biāo)準(zhǔn)適用于輕小型多旋翼無(wú)人機(jī)（起飛重量在 0.25kg～150kg 之間 ）的飛行控制與導(dǎo)航系統(tǒng)設(shè)計(jì)與制造。 其他無(wú)人機(jī)飛行控制與導(dǎo)航系統(tǒng)可參照?qǐng)?zhí)行。
General requirements for the flight control and navigation system of small and light multi-rotor unmanned aircraft
- ICS
- 49.090
- CCS
- V37
- 發(fā)布
- 2020-07-21
- 實(shí)施
- 2021-02-01 00:00:00.0
本標(biāo)準(zhǔn)規(guī)定了民用輕小型無(wú)人直升機(jī)飛行控制系統(tǒng)的通用要求、驗(yàn)證試驗(yàn)、標(biāo)識(shí)、包裝、運(yùn)輸和儲(chǔ)存。 本標(biāo)準(zhǔn)適用于民用輕小型無(wú)人直升機(jī)（起飛重量在 0.25kg～150kg 之間 ）飛行控制系統(tǒng)及其部件的設(shè)計(jì)與驗(yàn)證。 其他無(wú)人駕駛航空器飛行控制系統(tǒng)可參照?qǐng)?zhí)行。
General requirements for flight control systems of civil small and light unmanned helicopter
- ICS
- 49.090
- CCS
- V37
- 發(fā)布
- 2020-07-21
- 實(shí)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
- 發(fā)布
- 2021-04-00
- 實(shí)施
Small craft. Hydraulic steering systems
- ICS
- 47.020.70;47.080
- CCS
- V37
- 發(fā)布
- 2017-12-13
- 實(shí)施
- 2017-12-13
Space systems. Programme management. Management of product characteristics
- ICS
- 49.140
- CCS
- V37
- 發(fā)布
- 2017-03-31
- 實(shí)施
- 2017-03-31
Space systems - Debris mitigation design and operation manual for launch vehicle orbital stages
- ICS
- 49.140
- CCS
- V37
- 發(fā)布
- 2017-02-01
- 實(shí)施
Space product assurance - Storage, handling and transportation of spacecraft hardware; English version EN 16602-20-08:2016
- ICS
- 49.140
- CCS
- V37
- 發(fā)布
- 2016-12
- 實(shí)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
- 發(fā)布
- 2015-12-31
- 實(shí)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
- 發(fā)布
- 2015-10-15
- 實(shí)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
- 發(fā)布
- 2015-10
- 實(shí)施
本標(biāo)準(zhǔn)規(guī)定了民用飛機(jī)飛行控制系統(tǒng)(以下簡(jiǎn)稱(chēng)飛行控制系統(tǒng))模擬器試驗(yàn)、地面綜合試驗(yàn)和機(jī)上地面試驗(yàn)等地面試驗(yàn)的要求。 本標(biāo)準(zhǔn)適用于民用飛機(jī)飛行控制系統(tǒng)的地面試驗(yàn)。
Ground test requirements for flight control system of civil aircraft
- ICS
- 49.090
- CCS
- V37
- 發(fā)布
- 2014-05-19
- 實(shí)施
- 2014-10-01
本標(biāo)準(zhǔn)規(guī)定了民用飛機(jī)飛行控制系統(tǒng)(以下簡(jiǎn)稱(chēng)飛行控制系統(tǒng))的安全性設(shè)計(jì)、適航性設(shè)計(jì)、可靠性設(shè)計(jì)、維修性設(shè)計(jì)、系統(tǒng)安裝和主飛行控制系統(tǒng)設(shè)計(jì)、輔助飛行控制系統(tǒng)設(shè)計(jì)、自動(dòng)飛行控制系統(tǒng)設(shè)計(jì)等設(shè)計(jì)和安裝要求。 本標(biāo)準(zhǔn)適用于民用飛機(jī)飛行控制系統(tǒng)的研制。
Design and installation requirements for flight control system of civil aircraft
- ICS
- 49.090
- CCS
- V37
- 發(fā)布
- 2014-05-19
- 實(shí)施
- 2014-10-01
本標(biāo)準(zhǔn)規(guī)定了民用飛機(jī)飛行控制系統(tǒng)飛行試驗(yàn)的內(nèi)容和要求。 本標(biāo)準(zhǔn)適用于民用運(yùn)輸類(lèi)飛機(jī)電傳飛行控制系統(tǒng)的飛行試驗(yàn)。其他類(lèi)飛機(jī)可參照使用。
Requirements for flight test of civil aircraft flight control system
- ICS
- 49.020
- CCS
- V37
- 發(fā)布
- 2014-05-19
- 實(shí)施
- 2014-10-01
本標(biāo)準(zhǔn)規(guī)定了民用飛機(jī)飛行控制系統(tǒng)(以下簡(jiǎn)稱(chēng)飛行控制系統(tǒng))的尺寸、重量、材料、性能、環(huán)境適應(yīng)性、電磁兼容性、安全性、可靠性、維修性、測(cè)試性、互換性等技術(shù)要求以及相應(yīng)的驗(yàn)證要求。 本標(biāo)準(zhǔn)適用于民用飛機(jī)飛行控制系統(tǒng)的研制。
General requirements for flight control system of civil aircraft
- ICS
- 49.090
- CCS
- V37
- 發(fā)布
- 2014-05-19
- 實(shí)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
- 發(fā)布
- 2014-02-03
- 實(shí)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
- 發(fā)布
- 2013-02-11
- 實(shí)施
