摘要:
[Problem] Provided is a lock control device of a drive gear designed to ensure that a gear train is unlocked even if a load is applied to the drive gear, in the gear train in which the drive gear configured to drive a target object is locked by an idler gear and a lock gear. [Solution] For a gear train GL including a drive gear 33 and an idler gear 34 engaged with each other and a lock gear 35 capable of moving along an axis parallel to axes of the both gears 33 and 34, where the drive gear 33 is locked when the lock gear 35 is simultaneously engaged with the both gears 33 and 34 and the drive gear 33 is unlocked when the lock gear 35 is disengaged from the drive gear 33, provided are a first drive means 3A configured to linearly drive the lock gear 35 in forward and backward directions, a second drive means 3B configured to rotationally drive the drive gear 33 in normal and reverse directions, and a controller C configured to control the both drive means 3A and 3B. The controller C is configured to start driving the lock gear 35 at the time of an unlocking operation, from an engagement position toward the disengagement position through the first drive means 3A, and when the drive is started, the controller C drives the drive gear 33 into one of normal and reverse directions and into the other direction through the second drive means 3B with a polarity reversal in a predetermined cycles T1 and T2.
摘要:
A system comprising an aerial vehicle or an unmanned aerial vehicle (UAV) (100,400,1000,1500) configured to control pitch, roll, and/or yaw via airfoils (141,142,1345,1346) having resiliently mounted trailing edges opposed by fuselage-house deflecting actuator horns (621,622). Embodiments include one or more rudder elements (1045,1046,1145,1146,1245,1345,1346,1445,1446,1545,1546) which may be rotatably attached and actuated by an effector member (1049,1149,1249,1349) disposed within the fuselage housing (1001) and extendible in part to engage the one or more rudder elements.
摘要:
Die Erfindung betrifft ein Verfahren zum Schützen eines Fahrzeugs vor einem Angriff durch einen von einer Laserquelle ausgehenden Laserstrahl. Es wird vorgeschlagen, dass die Position der Laserquelle bestimmt wird und ein Lenkflugkörper gestartet und zur Laserquelle gelenkt wird.
摘要:
Die Erfindung geht aus von einem Verfahren zum Schützen eines Fahrzeugs (2) vor einem Angriff durch einen Laserstrahl (8). Ein effektiver Schutz kann erreicht werden, wenn ein Sensorsystem (14) Laserstrahlung des Laserstrahls (8) detektiert, und ein Lenkflugkörper (12, 14) in den Laserstrahl (8) hinein fliegt und das Fahrzeug (2) hierdurch abschattet.
摘要:
The present invention relates to electro-optic guided missile systems and, in particular, it concerns systems and methods providing enhanced navigation capabilities based on ego-motion processing of seeker images. The missile system comprising: a missile;a seeker located at a nose portion of said missile, said seeker comprising an electro-optic imaging sensor; and a control arrangement for steering the missile along a flight path to a target, characterized in that the missile system further comprises: a navigation subsystem receiving images from said imaging sensor, said navigation subsystem being configured to: co-process a plurality of said images from said imaging sensor to derive ego-motion of said missile relative to a region viewed by said imaging sensor;derive from said ego-motion a calculated target direction from said missile to a target.