RU94042469A - Устройство управления - Google Patents

Устройство управления

Info

Publication number
RU94042469A
RU94042469A RU94042469/02A RU94042469A RU94042469A RU 94042469 A RU94042469 A RU 94042469A RU 94042469/02 A RU94042469/02 A RU 94042469/02A RU 94042469 A RU94042469 A RU 94042469A RU 94042469 A RU94042469 A RU 94042469A
Authority
RU
Russia
Prior art keywords
control
rocket
flight
control system
controlling
Prior art date
Application number
RU94042469/02A
Other languages
English (en)
Inventor
Рансом Штефен
Gb]
Релотиус Клаус-Дитер
De]
Original Assignee
Эрно Раумфарттехник ГмбХ (DE)
Эрно Раумфарттехник ГмбХ
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Эрно Раумфарттехник ГмбХ (DE), Эрно Раумфарттехник ГмбХ filed Critical Эрно Раумфарттехник ГмбХ (DE)
Publication of RU94042469A publication Critical patent/RU94042469A/ru

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/002—Launch systems
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/40—Arrangements or adaptations of propulsion systems
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/002—Launch systems
    • B64G1/008—Arrangement of launch rockets or boosters
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/36—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
    • F42B10/60—Steering arrangements
    • F42B10/62—Steering by movement of flight surfaces
    • F42B10/64—Steering by movement of flight surfaces of fins

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Fluid Mechanics (AREA)
  • Physics & Mathematics (AREA)
  • General Engineering & Computer Science (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Transmission Devices (AREA)

Abstract

Устройство предназначено для управления поведением в полете ракеты-носителя, которая оснащена приводом, а также полезным грузом. Ракета-носитель имеет по меньшей мере одну систему управления, а также по меньшей мере один элемент управления для изменения траектории полета поперек продольной оси ракеты. Элемент управления выполнен в виде установленного с возможностью поворота управляющего крыла, которое расположено в боковой зоне ракеты-носителя. С управляющим крылом соединен исполнительный элемент, который настраивается системой управления таким образом, что подготовленные чувствительными элементами результаты измерения нагрузок боковым ветром преобразуются, с целью компенсации поперечных сил, в установку в заданное положение управляющего крыла.

Claims (1)

  1. Устройство предназначено для управления поведением в полете ракеты-носителя, которая оснащена приводом, а также полезным грузом. Ракета-носитель имеет по меньшей мере одну систему управления, а также по меньшей мере один элемент управления для изменения траектории полета поперек продольной оси ракеты. Элемент управления выполнен в виде установленного с возможностью поворота управляющего крыла, которое расположено в боковой зоне ракеты-носителя. С управляющим крылом соединен исполнительный элемент, который настраивается системой управления таким образом, что подготовленные чувствительными элементами результаты измерения нагрузок боковым ветром преобразуются, с целью компенсации поперечных сил, в установку в заданное положение управляющего крыла.
RU94042469/02A 1993-01-14 1994-01-13 Устройство управления RU94042469A (ru)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DEP4300761.9 1993-01-14
DE4300761A DE4300761A1 (de) 1993-01-14 1993-01-14 Vorrichtung zur Steuerung

Publications (1)

Publication Number Publication Date
RU94042469A true RU94042469A (ru) 1996-09-10

Family

ID=6478151

Family Applications (1)

Application Number Title Priority Date Filing Date
RU94042469/02A RU94042469A (ru) 1993-01-14 1994-01-13 Устройство управления

Country Status (7)

Country Link
US (1) US5593110A (ru)
EP (1) EP0632879A1 (ru)
JP (1) JPH07507521A (ru)
CN (1) CN1107114A (ru)
DE (1) DE4300761A1 (ru)
RU (1) RU94042469A (ru)
WO (1) WO1994016286A1 (ru)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2000029805A1 (fr) * 1998-11-13 2000-05-25 Mashinostroitelnoe Konstruktorskoe Bjuro 'fakel' Dispositif de commande de missile de grande manoeuvrabilite

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GB2342145B (en) * 1998-08-29 2002-07-31 Marconi Gec Ltd Control system
US6685143B1 (en) * 2003-01-03 2004-02-03 Orbital Research Inc. Aircraft and missile forebody flow control device and method of controlling flow
US8047472B1 (en) * 2006-06-06 2011-11-01 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Ram booster
US7781709B1 (en) * 2008-05-05 2010-08-24 Sandia Corporation Small caliber guided projectile
US8424808B2 (en) 2009-06-15 2013-04-23 Blue Origin, Llc Compensating for wind prior to engaging airborne propulsion devices
US8729442B2 (en) * 2009-06-15 2014-05-20 Blue Origin, Llc Predicting and correcting trajectories
CN101694364B (zh) * 2009-09-30 2012-09-26 北京航天自动控制研究所 摄动制导与迭代制导的快速转换方法
CN101672606B (zh) * 2009-09-30 2012-09-26 北京航天自动控制研究所 一种运载火箭的导引控制方法
CN101723096B (zh) * 2009-12-24 2013-05-01 北京航天自动控制研究所 迭代制导下减少大姿态扰动的控制方法
CN106500550A (zh) * 2016-12-15 2017-03-15 福州幻科机电科技有限公司 带有遥控滑翔翼尾舵翼的逃逸塔整流罩助推火箭
CN107063006B (zh) * 2017-04-03 2018-11-27 湖北航天技术研究院总体设计所 一种可重复使用航天运载系统及往返方法
CN107628274B (zh) * 2017-09-20 2019-10-11 北京航空航天大学 利用火箭发动机燃气的姿态控制装置和姿态控制系统
US11535403B1 (en) * 2018-11-14 2022-12-27 CubeCab Inc. Customization and automation of launch vehicle
CN113790636B (zh) * 2021-08-31 2024-04-09 北京航空航天大学 一种采用卷弧翼实现滑翔增程及精确控制的火箭
CN114413690B (zh) * 2022-01-18 2024-04-05 南京理工大学 一种用于火箭一子级落区控制的修正系统及方法

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US3000597A (en) * 1951-08-15 1961-09-19 Alfred J Bell Rocket-propelled missile
US3708139A (en) * 1959-01-19 1973-01-02 Us Navy Missile control system
US3233848A (en) * 1959-09-17 1966-02-08 Motorola Inc Guidance system with a free falling mass
GB982779A (en) * 1962-07-10 1965-02-10 English Electric Co Ltd Improvements in or relating to aerial vehicles
US3636877A (en) * 1964-06-02 1972-01-25 Us Navy Antisubmarine missile
US3568954A (en) * 1966-04-04 1971-03-09 William C Mccorkle Jr Directional control-automatic meteorological compensation (d.c.-automet) inertial guidance system for artillery missiles
US3464649A (en) * 1967-12-20 1969-09-02 Us Army Missile system with heading plus drift control
GB1269272A (en) * 1968-06-06 1972-04-06 Messeschmitt Bolkow Blohm Gmbh Improvements in multi-stage rockets
US3945588A (en) * 1973-06-18 1976-03-23 Maglio Jr Melvin R Anti-tank missile
US4023749A (en) * 1975-12-08 1977-05-17 The United States Of America As Represented By The Secretary Of The Army Directional control system for artillery missiles
US4364530A (en) * 1980-09-08 1982-12-21 The United States Of America As Represented By The Secretary Of The Navy Propulsion/control modular booster
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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2000029805A1 (fr) * 1998-11-13 2000-05-25 Mashinostroitelnoe Konstruktorskoe Bjuro 'fakel' Dispositif de commande de missile de grande manoeuvrabilite

Also Published As

Publication number Publication date
JPH07507521A (ja) 1995-08-24
WO1994016286A1 (de) 1994-07-21
EP0632879A1 (de) 1995-01-11
US5593110A (en) 1997-01-14
CN1107114A (zh) 1995-08-23
DE4300761A1 (de) 1994-07-21

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