WO2012041097A1 - 一种低空慢速小目标的拦截方法 - Google Patents

一种低空慢速小目标的拦截方法 Download PDF

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Publication number
WO2012041097A1
WO2012041097A1 PCT/CN2011/076629 CN2011076629W WO2012041097A1 WO 2012041097 A1 WO2012041097 A1 WO 2012041097A1 CN 2011076629 W CN2011076629 W CN 2011076629W WO 2012041097 A1 WO2012041097 A1 WO 2012041097A1
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WIPO (PCT)
Prior art keywords
target
low
intercepting
altitude
control device
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PCT/CN2011/076629
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English (en)
French (fr)
Inventor
刘浩
王生捷
丁旭昶
魏小鸣
韩书永
邱旭阳
迟克刚
申研
陈爱锋
唐玉龙
Original Assignee
北京机械设备研究所
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Application filed by 北京机械设备研究所 filed Critical 北京机械设备研究所
Priority to EP11827993.4A priority Critical patent/EP2623921B1/en
Priority to JP2013529535A priority patent/JP5603497B2/ja
Publication of WO2012041097A1 publication Critical patent/WO2012041097A1/zh
Priority to US13/851,101 priority patent/US8550346B2/en

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Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G3/00—Aiming or laying means
    • F41G3/06—Aiming or laying means with rangefinder
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G3/00—Aiming or laying means
    • F41G3/14—Indirect aiming means
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41G—WEAPON SIGHTS; AIMING
    • F41G5/00—Elevating or traversing control systems for guns
    • F41G5/08—Ground-based tracking-systems for aerial targets
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41H—ARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
    • F41H11/00—Defence installations; Defence devices
    • F41H11/02—Anti-aircraft or anti-guided missile or anti-torpedo defence installations or systems
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41H—ARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
    • F41H13/00—Means of attack or defence not otherwise provided for
    • F41H13/0006—Ballistically deployed systems for restraining persons or animals, e.g. ballistically deployed nets

Definitions

  • the invention relates to an intercepting method for an air target, in particular to an intercepting method for a low altitude slow small target.
  • non-lethal weapon at home and abroad that is a network capture system.
  • the existing network capture systems at home and abroad are aimed at ground targets.
  • the domestic use of police 'net guns' to intercept targets is mainly used in Ukraine.
  • the ' ⁇ ' system captures the target.
  • the 'net gun' uses high-pressure gas or an empty bomb as a power to throw and open the catching net to capture criminals.
  • the Ukrainian ' ⁇ ' system can launch a capture network at a greater distance to capture ground targets. Both of these methods are non-killing mesh intercept methods, which are mainly used to capture ground targets and are powerless to capture aerial targets.
  • the object of the present invention is to provide an intercepting method for a low-altitude slow small target, which solves the problem that the existing method for capturing a ground target is incapable of capturing an air target.
  • the intercepting method of a low-altitude slow small target is realized by the following components, and the components include: a detecting device, an accusation device, an aiming control device, a launching device, a transmitting device, and an intercepting device.
  • a specific step of a low-altitude slow small target interception method is:
  • the operator observes through the visual observation and finds that there are low-altitude slow small targets nearby, tracking the low-altitude slow small targets through the sights on the aiming device, and measuring the azimuth, altitude and speed of the target in real time by laser ranging. Parameters.
  • the airborne domain is searched by the detecting device, the target is identified according to the detecting device, the low-altitude slow small target is identified, the low-altitude slow small target is tracked, and the target's azimuth, altitude and speed are measured by laser ranging. Parameters.
  • the second step is to solve the ballistics and aim at the target.
  • the control device performs the ballistic solution in real time according to the target parameter. After the solution is successful, for the individual soldier mode, the operation target uses the shooting preset point displayed by the aiming control device to aim at the target. For the networking mode, the control device performs ballistic solution in real time and controls the corresponding transmitting device to align the target in real time.
  • the formula for the ballistic solution is as follows:
  • the third step is to bind the parameters and launch the intercepting device.
  • control device calculates the opening time, and binds the opening time to the intercepting device and transmits the intercepting device by the transmitting device.
  • the fourth step is to shoot the interception network and intercept the target.
  • the interception device After the interception device is launched into space, it will fly according to the predetermined ballistics. When it reaches the target position, it will eject the intercepting net, intercept the net and fly to the target, and after hitting the target, wrap the target, causing the target to lose power and fall.
  • Step 5 Open the parachute and carry the remaining load to land
  • the intercepting device opens the parachute, and the residual load of the parachute carrying the intercepting device drops to the ground at a speed of 4 m/s to 8 m/s.
  • the method is to capture an air target from a ground launch intercepting device, and has the advantages of low cost, short reaction time, and deceleration of residual load, and is suitable for use in an urban environment.
  • the intercepting method of a low-altitude slow small target is realized by the following components, and the components include: a detecting device, an accusation device, an aiming control device, a launching device, a transmitting device, and an intercepting device.
  • a specific step of a low-altitude slow small target interception method is:
  • the operator observes through the visual observation and finds that there are low-altitude slow small targets nearby, tracking the low-altitude slow small targets through the sights on the aiming device, and measuring the azimuth, altitude and speed of the target in real time by laser ranging. Parameters.
  • the airborne domain is searched by the detecting device, the target is identified according to the detecting device, the low-altitude slow small target is identified, the low-altitude slow small target is tracked, and the target's azimuth, altitude and speed are measured by laser ranging. Parameters.
  • the second step is to solve the ballistics and aim at the target.
  • the control device performs the ballistic solution in real time according to the target parameter. After the solution is successful, for the individual soldier mode, the operation target uses the shooting preset point displayed by the aiming control device to aim at the target. For the networking mode, the control device performs ballistic solution in real time and controls the corresponding transmitting device to align the target in real time.
  • the formula for the ballistic solution is as follows:
  • the third step is to bind the parameters and launch the intercepting device.
  • control device calculates the opening time, and binds the opening time to the intercepting device and transmits the intercepting device by the transmitting device.
  • the fourth step is to shoot the interception network and intercept the target.
  • the interception device After the interception device is launched into space, it will fly according to the predetermined ballistics. When it reaches the target position, it will eject the intercepting net, intercept the net and fly to the target, and after hitting the target, wrap the target, causing the target to lose power and fall.
  • Step 5 Open the parachute and carry the remaining load to land
  • the intercepting device opens the parachute, and the residual load of the parachute carrying the intercepting device drops to the ground at a speed of 4 m/s to 8 m/s.
  • the intercepting method of the low-altitude slow small target is realized by the following components, and the composition includes: an aiming control device, a launching device, a transmitting device, and an intercepting device.
  • the specific steps of the low-altitude slow target interception method are:
  • the operator searches and tracks the target through the aiming device, and uses laser ranging to measure the target's azimuth, altitude, speed and other parameters in real time.
  • the second step is to solve the ballistics and aim at the target.
  • the control device performs the ballistic solution in real time according to the target parameter. After the solution is successful, the operation target uses the shooting preset position displayed by the aiming control device to aim at the target.
  • the formula for the ballistic solution is as follows:
  • the third step is to bind the parameters and launch the intercepting device.
  • control device calculates the opening time, and binds the opening time to the intercepting device and transmits the intercepting device by the transmitting device.
  • the fourth step is to shoot the interception network and intercept the target.
  • the interception device After the interception device is launched into space, it will fly according to the predetermined ballistics. When it reaches the target position, it will eject the intercepting net, intercept the net and fly to the target, and after hitting the target, wrap the target, causing the target to lose power and fall.
  • Step 5 Turn on the parachute and carry the remaining load at a low speed.
  • the interceptor opens the parachute and the remaining load of the parachute carrying the interceptor drops to the ground at a speed of 6 m/s.
  • the intercepting method of the low-altitude slow small target is realized by the following components, and the components include: a detecting device, an accusation device, a dispatching device, a transmitting device, and an intercepting device.
  • the airborne domain is searched by the detecting device, the target is identified according to the detecting device, the low-altitude slow small target is identified, the low-altitude slow small target is tracked, and the target azimuth, altitude and speed parameters are measured in real time by laser ranging.
  • the second step is to solve the ballistics and aim at the target.
  • the accusation device processes the target information according to the detection device and sends it to the control device, and the control device performs the ballistic solution in real time, and controls the corresponding transmitting device to align the target in real time.
  • the formula for the ballistic solution is as follows:
  • the third step is to bind the parameters and launch the intercepting device.
  • control device calculates the opening time, and binds the opening time to the intercepting device and transmits the intercepting device.
  • the fourth step is to shoot the interception network and intercept the target.
  • the interception device After the interception device is launched into space, it will fly according to the predetermined ballistics. When it reaches the target position, it will eject the intercepting net, intercept the net and fly to the target, and after hitting the target, wrap the target, causing the target to lose power and fall.
  • Step 5 Open the parachute and carry the remaining load at low speed.
  • the interceptor opens the parachute and the remaining load of the parachute carrying the interceptor drops to the ground at a speed of 6 m/s.
  • the method is to capture an air target from a ground launch intercepting device, and has the advantages of low cost, short reaction time, and deceleration of residual load, and is suitable for use in an urban environment.

Description

一种低空慢速小目标的拦截方法 Technical Field
本发明涉及一种空中目标的拦截方法，特别是一种低空慢速小目标的拦截方法。
Background Art
近年来针对城市大型集会、大型活动，安保工作的一大主要任务是防止恐怖主义分子或敌对分子利用航模、气球等低空慢速小型飞行器进行破坏活动。由于是城市环境以及大型活动的特殊性，针对低空慢速小目标的拦截，不能使用现有的防空武器和枪支等杀伤性武器，必须选择非杀伤性的拦截方式。
目前国内外非杀伤性武器有一类是网式捕捉系统，国内外现有的网式捕捉系统均是针对地面目标，国内主要采用警用'网枪'来拦截目标的方法，国外主要采用乌克兰的'КОБА'系统捕捉目标的方法。 '网枪'是利用高压气体或空包弹作为动力将捕捉网抛出并打开来捕捉犯罪分子。乌克兰'КОБА'系统可在较远距离发射捕捉网捕捉地面目标。这两种方法都是非杀伤性的网式拦截方法，作用主要是捕捉地面目标，对捕捉空中目标无能为力。
 Technical Problem
本发明的目的在于提供一种低空慢速小目标的拦截方法，解决现有捕捉地面目标方法对捕捉空中目标无能为力的问题。
Technical Solution
一种低空慢速小目标的拦截方法是通过以下组成实现的，组成包括：探测设备、指控设备、瞄控设备、发控设备、发射装置和拦截装置。
一种低空慢速小目标拦截方法的具体步骤为：
第一步 探测目标
对于单兵模式，操作手通过目测观察，发现附近有低空慢速小目标时，通过瞄控设备上的瞄准器跟踪低空慢速小目标，并采用激光测距实时测量目标的方位、高度、速度的参数。
对于联网模式，通过探测设备对空域进行搜索，根据探测设备对目标进行识别，识别出低空慢速小目标后，跟踪低空慢速小目标，并采用激光测距实时测量目标的方位、高度、速度的参数。
第二步 解算弹道，对准目标
发控设备根据目标参数实时进行弹道解算，解算成功后，对于单兵模式，操作手用瞄控设备显示的射击预置点瞄准目标。对于联网模式，发控设备实时进行弹道解算，并控制相应的发射装置实时对准目标。弹道解算的公式如下：
Figure PCTCN2011076629-appb-M000001
Figure PCTCN2011076629-appb-M000002
Figure PCTCN2011076629-appb-M000003
Figure PCTCN2011076629-appb-M000004
Figure PCTCN2011076629-appb-M000005
Figure PCTCN2011076629-appb-M000006
Figure PCTCN2011076629-appb-M000007
Figure PCTCN2011076629-appb-M000008
Figure PCTCN2011076629-appb-M000009
Figure PCTCN2011076629-appb-M000010
Figure PCTCN2011076629-appb-M000011
第三步 装订参数，发射拦截装置
发控设备对弹道解算完成后，计算出开网时间，并将开网时间装订到拦截装置上并由发射装置发射拦截装置。
第四步 抛射拦截网，拦截目标
拦截装置发射升空后按照预定的弹道飞行，飞至目标位置时抛射拦截网，拦截网飞向目标，碰到目标后缠绕目标，使目标失去动力而坠落。
第五步 打开降落伞，携带剩余载荷降落
拦截装置打开降落伞，降落伞携带拦截装置的剩余载荷以4m/s～8m/s的速度降落至地面。
至此，完成低空慢速小目标的拦截。
 Advantageous Effects
本方法是从地面发射拦截装置捕捉空中目标，具有成本低、反应时间短、剩余载荷减速下落的优点，适合在城市环境使用。
Best Mode
一种低空慢速小目标的拦截方法是通过以下组成实现的，组成包括：探测设备、指控设备、瞄控设备、发控设备、发射装置和拦截装置。
一种低空慢速小目标拦截方法的具体步骤为：
第一步 探测目标
对于单兵模式，操作手通过目测观察，发现附近有低空慢速小目标时，通过瞄控设备上的瞄准器跟踪低空慢速小目标，并采用激光测距实时测量目标的方位、高度、速度的参数。
对于联网模式，通过探测设备对空域进行搜索，根据探测设备对目标进行识别，识别出低空慢速小目标后，跟踪低空慢速小目标，并采用激光测距实时测量目标的方位、高度、速度的参数。
第二步 解算弹道，对准目标
发控设备根据目标参数实时进行弹道解算，解算成功后，对于单兵模式，操作手用瞄控设备显示的射击预置点瞄准目标。对于联网模式，发控设备实时进行弹道解算，并控制相应的发射装置实时对准目标。弹道解算的公式如下：
Figure PCTCN2011076629-appb-M000012
Figure PCTCN2011076629-appb-M000013
Figure PCTCN2011076629-appb-M000014
Figure PCTCN2011076629-appb-M000015
Figure PCTCN2011076629-appb-M000016
Figure PCTCN2011076629-appb-M000017
Figure PCTCN2011076629-appb-M000018
Figure PCTCN2011076629-appb-M000019
Figure PCTCN2011076629-appb-M000020
Figure PCTCN2011076629-appb-M000021
Figure PCTCN2011076629-appb-M000022
第三步 装订参数，发射拦截装置
发控设备对弹道解算完成后，计算出开网时间，并将开网时间装订到拦截装置上并由发射装置发射拦截装置。
第四步 抛射拦截网，拦截目标
拦截装置发射升空后按照预定的弹道飞行，飞至目标位置时抛射拦截网，拦截网飞向目标，碰到目标后缠绕目标，使目标失去动力而坠落。
第五步 打开降落伞，携带剩余载荷降落
拦截装置打开降落伞，降落伞携带拦截装置的剩余载荷以4m/s～8m/s的速度降落至地面。
至此，完成低空慢速小目标的拦截。
 Mode for Invention
在单兵模式下，低空慢速小目标的拦截方法是通过以下组成实现的，组成包括：瞄控设备、发控设备、发射装置和拦截装置。
在单兵模式下，低空慢速小目标的拦截方法的具体步骤为：
第一步 探测目标
操作手通过瞄控设备搜索、跟踪目标，并采用激光测距实时测量目标的方位、高度、速度等参数。
第二步 解算弹道，对准目标
发控设备根据目标参数实时进行弹道解算，解算成功后，操作手用瞄控装置显示的射击预置点瞄准目标。弹道解算的公式如下：
Figure PCTCN2011076629-appb-M000023
Figure PCTCN2011076629-appb-M000024
Figure PCTCN2011076629-appb-M000025
Figure PCTCN2011076629-appb-M000026
Figure PCTCN2011076629-appb-M000027
Figure PCTCN2011076629-appb-M000028
Figure PCTCN2011076629-appb-M000029
Figure PCTCN2011076629-appb-M000030
Figure PCTCN2011076629-appb-M000031
Figure PCTCN2011076629-appb-M000032
Figure PCTCN2011076629-appb-M000033
第三步 装订参数，发射拦截装置
发控设备对弹道解算完成后，计算出开网时间，并将开网时间装订到拦截装置上并由发射装置发射拦截装置。
第四步 抛射拦截网，拦截目标
拦截装置发射升空后按照预定的弹道飞行，飞至目标位置时抛射拦截网，拦截网飞向目标，碰到目标后缠绕目标，使目标失去动力而坠落。
第五步 打开降落伞，携带剩余载荷低速降落。
拦截装置打开降落伞，降落伞携带拦截装置的剩余载荷以 6m/s 的速度降落至地面。
至此完成单兵模式下低空慢速小目标的拦截。
具体实施方式 2
在联网模式下，低空慢速小目标的拦截方法是通过以下组成实现的，组成包括：探测设备、指控设备、发控设备、发射装置和拦截装置。
在联网模式下，低空慢速小目标的拦截方法的具体步骤为：
第一步 探测目标
通过探测设备对空域进行搜索，根据探测设备对目标进行识别，识别出低空慢速小目标后，跟踪低空慢速小目标，并采用激光测距实时测量目标的方位、高度、速度的参数。
第二步 解算弹道，对准目标
指控设备根据探测装置提供的目标信息处理后发送给发控设备，发控设备实时进行弹道解算，并控制相应的发射装置实时对准目标。弹道解算的公式如下：
Figure PCTCN2011076629-appb-M000034
Figure PCTCN2011076629-appb-M000035
Figure PCTCN2011076629-appb-M000036
Figure PCTCN2011076629-appb-M000037
Figure PCTCN2011076629-appb-M000038
Figure PCTCN2011076629-appb-M000039
Figure PCTCN2011076629-appb-M000040
Figure PCTCN2011076629-appb-M000041
Figure PCTCN2011076629-appb-M000042
Figure PCTCN2011076629-appb-M000043
Figure PCTCN2011076629-appb-M000044
第三步 装订参数，发射拦截装置
当弹道解算成功时，发控设备计算出开网时间，并将开网时间装订到拦截装置并发射拦截装置。
第四步 抛射拦截网，拦截目标
拦截装置发射升空后按照预定的弹道飞行，飞至目标位置时抛射拦截网，拦截网飞向目标，碰到目标后缠绕目标，使目标失去动力而坠落。
第五步 打开降落伞，携带剩余载荷低速降落
拦截装置打开降落伞，降落伞携带拦截装置的剩余载荷以6m/s 的速度降落至地面。
至此完成在联网模式下低空慢速小目标的拦截。
Industrial Applicability
本方法是从地面发射拦截装置捕捉空中目标，具有成本低、反应时间短、剩余载荷减速下落的优点，适合在城市环境使用。
Sequence List Text

Claims (1)

1. 一种低空慢速小目标的拦截方法，是通过以下组成实现的，组成包括：探测设备、指控设备、瞄控设备、发控设备、发射装置和拦截装置；
其特征在于本方法的具体步骤为：
第一步 探测目标
对于单兵模式，操作手通过目测观察，发现附近有低空慢速小目标时，通过瞄控装置上的瞄准器跟踪低空慢速小目标，并采用激光测距实时测量目标的方位、高度、速度的参数；
对于联网模式，通过探测设备对空域进行搜索，根据探测设备对目标进行识别，识别出低空慢速小目标后，跟踪低空慢速小目标，并采用激光测距实时测量目标的方位、高度、速度的参数；
第二步 解算弹道，对准目标
发控设备根据目标参数实时进行弹道解算，解算成功后，对于单兵模式，操作手用瞄控装置显示的射击预置点瞄准目标；对于联网模式，发控设备实时进行弹道解算，并控制相应的发射装置实时对准目标；弹道解算的公式如下：
Figure PCTCN2011076629-appb-M000045
Figure PCTCN2011076629-appb-M000046
Figure PCTCN2011076629-appb-M000047
Figure PCTCN2011076629-appb-M000048
Figure PCTCN2011076629-appb-M000049
Figure PCTCN2011076629-appb-M000050
Figure PCTCN2011076629-appb-M000051
Figure PCTCN2011076629-appb-M000052
Figure PCTCN2011076629-appb-M000053
Figure PCTCN2011076629-appb-M000054
Figure PCTCN2011076629-appb-M000055
第三步 装订参数，发射拦截装置
发控设备对弹道解算完成后，计算出开网时间，并将开网时间装订到拦截装置上并由发射装置发射拦截装置；
第四步 抛射拦截网，拦截目标
拦截装置发射升空后按照预定的弹道飞行，飞至目标位置时抛射拦截网，拦截网飞向目标，碰到目标后缠绕目标，使目标失去动力而坠落；
第五步 打开降落伞，携带剩余载荷降落
拦截装置打开降落伞，降落伞携带拦截装置的剩余载荷以4m/s～8m/s的速度降落至地面;
至此，完成低空慢速小目标的拦截。
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Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101982720B (zh) * 2010-09-29 2012-11-14 北京机械设备研究所 一种低空慢速小目标的拦截方法
CN102087082B (zh) 2010-11-22 2013-05-08 北京机械设备研究所 一种基于射表拟合的低空慢速小目标拦截方法
CN102261869A (zh) * 2011-06-15 2011-11-30 北京机械设备研究所 一种拦截低空慢速小目标单兵数字化火控装置
CN103134387B (zh) * 2011-11-29 2014-10-15 北京航天长峰科技工业集团有限公司 一种低空慢速小目标探测与拦截系统标定方法
CN106017226B (zh) * 2012-07-22 2017-12-05 衢州市优德工业设计有限公司 一种陆基阵列式高能激光防空方法
CN104833968A (zh) * 2015-05-06 2015-08-12 长安大学 一种用于再入弹道目标跟踪的有限差分滤波方法
CN104880126B (zh) * 2015-05-19 2017-01-18 北京机械设备研究所 一种基于航迹外推的低慢小目标拦截方法
JP2017009244A (ja) * 2015-06-25 2017-01-12 株式会社ディスコ 小型無人飛行機撃退装置
CN105116916A (zh) * 2015-09-25 2015-12-02 北京机械设备研究所 一种分布式光电跟踪系统协同跟踪方法
CN105651120A (zh) * 2016-01-30 2016-06-08 上海仪耐新材料科技有限公司 一种固定式反无人机拦截网系统
CN106341206A (zh) * 2016-08-26 2017-01-18 广东容祺智能科技有限公司 一种低空无人机防御系统
CN106382857A (zh) * 2016-11-15 2017-02-08 成都赫尔墨斯科技有限公司 一种无人机拦截方法及系统
CN106643291B (zh) * 2016-12-26 2018-04-13 北京机械设备研究所 一种远距离高精度投弹式救援器材投送方法
CN106767172B (zh) * 2017-01-23 2018-04-03 芜湖博高光电科技股份有限公司 一种肩扛便携式反无人机弹射软毁伤回收装置
CN106679507B (zh) * 2017-01-23 2018-04-03 芜湖博高光电科技股份有限公司 一种软毁伤弹药
CN109684985A (zh) * 2018-12-19 2019-04-26 罗建葛 一种智能值守系统和值守方法
CN112361887B (zh) * 2020-11-09 2021-10-26 北京理工大学 一种针对近地目标拦截的发射窗口规划方法
CN113610896B (zh) * 2021-08-17 2022-09-02 北京波谱华光科技有限公司 一种简易火控瞄具中目标提前量测量方法及系统

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1527020A (zh) * 2003-03-05 2004-09-08 陈仰帆 一种自动攻击低空飞行器的方法及其火炮系统
WO2006079029A2 (en) * 2005-01-24 2006-07-27 Ron Allen Defense system and method
WO2008029392A2 (en) * 2006-09-03 2008-03-13 E.C.S. Engineering Consulting Services-Aerospace Ltd. Method and system for defense against incoming rockets and missiles
CN101392999A (zh) * 2007-09-18 2009-03-25 中国科学院力学研究所 航模拦截方法及装置
CN101982720A (zh) * 2010-09-29 2011-03-02 北京机械设备研究所 一种低空慢速小目标的拦截方法

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR812183A (fr) * 1936-09-26 1937-05-01 Obus pour le placement d'obstacles et de rideaux d'obstacles contre avions
US3892466A (en) * 1971-12-17 1975-07-01 Hughes Aircraft Co Laser-sight and computer for anti-aircraft gun fire control system
US4146780A (en) * 1976-12-17 1979-03-27 Ares, Inc. Antiaircraft weapons system fire control apparatus
SE441033B (sv) * 1978-11-02 1985-09-02 Barr & Stroud Ltd Eldledningsanordning for en kanon
DE2912587C1 (de) * 1979-03-30 1986-05-07 Siemens AG, 1000 Berlin und 8000 München Feuerleiteinrichtung,insbesondere fuer ein mobiles Flugabwehrsystem
CN85106886A (zh) * 1985-09-12 1987-03-11 康特拉弗斯有限公司 制止浮动目标用的弹头
FR2635379B1 (fr) * 1988-08-12 1993-11-12 Sagem Installation de conduite de tir a compensation des erreurs de pointage
FR2695467B1 (fr) * 1992-09-04 1994-10-21 Thomson Brandt Armements Procédé de neutralisation de cible aérienne évoluant à l'aide de pales et système et projectile pour la mise en Óoeuvre de ce procédé.
FR2712972B1 (fr) * 1993-11-25 1996-01-26 Aerospatiale Système de défense antiaérien et missile de défense pour un tel système.
DE4409424C1 (de) * 1994-03-18 1995-08-10 Daimler Benz Aerospace Ag Abfangvorrichtung für Flugobjekte
DE10024320C2 (de) * 2000-05-17 2002-09-05 Diehl Munitionssysteme Gmbh Radareinrichtung für den Objekt-Selbstschutz
US6626077B1 (en) * 2002-10-16 2003-09-30 Mark David Gilbert Intercept vehicle for airborne nuclear, chemical and biological weapons of mass destruction
US7190304B1 (en) * 2003-12-12 2007-03-13 Bae Systems Information And Electronic Systems Integration Inc. System for interception and defeat of rocket propelled grenades and method of use
WO2009104557A1 (ja) 2008-02-21 2009-08-27 株式会社カネカ Ｎ－（３－ピロリジニル）グリシン誘導体の製造法
US8375837B2 (en) * 2009-01-19 2013-02-19 Honeywell International Inc. Catch and snare system for an unmanned aerial vehicle
DE102009006498A1 (de) * 2009-01-28 2010-07-29 Krauss-Maffei Wegmann Gmbh & Co. Kg Cargo-Geschoss

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1527020A (zh) * 2003-03-05 2004-09-08 陈仰帆 一种自动攻击低空飞行器的方法及其火炮系统
WO2006079029A2 (en) * 2005-01-24 2006-07-27 Ron Allen Defense system and method
WO2008029392A2 (en) * 2006-09-03 2008-03-13 E.C.S. Engineering Consulting Services-Aerospace Ltd. Method and system for defense against incoming rockets and missiles
CN101392999A (zh) * 2007-09-18 2009-03-25 中国科学院力学研究所 航模拦截方法及装置
CN101982720A (zh) * 2010-09-29 2011-03-02 北京机械设备研究所 一种低空慢速小目标的拦截方法

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