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Hello, what are the control inputs required in a hover in an ideal
situation, what I am trying to figure out is what are you doing in a no-wind situation to hover. I have read several articles and books about helicopter flying and I am still a little confused as to what you have to do, from what I gather there is constant control inputs to fly a helicopter and that a helicopter is hover with its left skid low but at the same time I have hearing tokeep the helicopter in a level attitude, so how can that be. From what I gather so far, when you hover, you add left pedal, increase collective and power, then right cyclic; what I am wondering is what cues do you look for to determine what control inputs is needed and where are your eyes focused for all of this. I read an article in Avweb where the pilot was going to a higher helicopter rating and he asked a more experience pilot about the trouble he was having and the pilot told him to look up and after consideration from the less experience pilot that worked for him, so look up at what-- the rotor, something at eye level or not to look at the ground. What I am trying to determine here is how to hover a helicopter, what control inputs do you have to make and in what order, I have heard that once one control input is made you have to use all of the controls but dont you have to do it in a certain order and where and what are your eyes focused and what are the cues that you are looking for to determine which control input is needed. I am trying to determine the mechanics and the cues needed to hover. Thanks in advance for your response. |
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Wannafly wrote:
Hello, what are the control inputs required in a hover in an ideal situation, what I am trying to figure out is what are you doing in a no-wind situation to hover. I have read several articles and books about helicopter flying and I am still a little confused as to what you have to do, from what I gather there is constant control inputs to fly a helicopter and that a helicopter is hover with its left skid low but at the same time I have hearing tokeep the helicopter in a level attitude, so how can that be. From what I gather so far, when you hover, you add left pedal, increase collective and power, then right cyclic; what I am wondering is what cues do you look for to determine what control inputs is needed and where are your eyes focused for all of this. I read an article in Avweb where the pilot was going to a higher helicopter rating and he asked a more experience pilot about the trouble he was having and the pilot told him to look up and after consideration from the less experience pilot that worked for him, so look up at what-- the rotor, something at eye level or not to look at the ground. What I am trying to determine here is how to hover a helicopter, what control inputs do you have to make and in what order, I have heard that once one control input is made you have to use all of the controls but dont you have to do it in a certain order and where and what are your eyes focused and what are the cues that you are looking for to determine which control input is needed. I am trying to determine the mechanics and the cues needed to hover. Thanks in advance for your response. If anybody thinks they can explain in writing how to properly hover is full of crap. Remember the old video of the guy spinning plates on the the ends of multiple poles. That's what it is like to hover. |
#3
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![]() "Wannafly" wrote in message oups.com... Hello, what are the control inputs required in a hover in an ideal situation, what I am trying to figure out is what are you doing in a no-wind situation to hover. There's no other good answer to your question except: "The correct ones." I'm not being sarcastic, its just that your question is like asking "how to I ride a bicycle." The way you teach someone to hover is to give them each control one at a time while you describe what they're doing incorrectly (which is usually overcontrolling) and what they're doing correctly (usually very little at the start). The student just eventually figures it out during which time the instructor prevents expensive crashes. From experience I can tell you that IGE hovering does not become totally second nature for quite some time, my guess is a few hundred hours. Bart BTW: Happy New Years all you RAR fans, trolls, contributors, and lurkers! |
#4
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Hello, what are the control inputs required in a hover in an ideal
situation, what I am trying to figure out is what are you doing in a no-wind situation to hover. There's no other good answer to your question except: "The correct ones." I'm not being sarcastic, its just that your question is like asking "how to I ride a bicycle." I like this comparison. You can do both things only if you do not need to think about it. Maybe the original poster is confused about the theoretical basics. If you have ideal (theoretical) conditions you don't need to do anything. But this cannot happen in real life. If the slightest disturbance occurs (and if there are no external - like wind gusts - at all, the heli produces its own - always) the helicopter will move into one direction. Normal, simple helicopters then return to their initial position, and overshoot this position by more than the initial disturbance. This dynamic instability is inherent to helicopters with the main rotor center of thrust above the center of gravity and the rotor disc trying to keep its angle to the mast. |
#5
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![]() Think of it this way, the control imput you just made changed all the previous ones. So now that you did that you must readjust them all again. Then you have to do it over and over again untill its back on the skids in flat pitch. "Wannafly" wrote in message oups.com... Hello, what are the control inputs required in a hover in an ideal situation, what I am trying to figure out is what are you doing in a no-wind situation to hover. I have read several articles and books about helicopter flying and I am still a little confused as to what you have to do, from what I gather there is constant control inputs to fly a helicopter and that a helicopter is hover with its left skid low but at the same time I have hearing tokeep the helicopter in a level attitude, so how can that be. From what I gather so far, when you hover, you add left pedal, increase collective and power, then right cyclic; what I am wondering is what cues do you look for to determine what control inputs is needed and where are your eyes focused for all of this. I read an article in Avweb where the pilot was going to a higher helicopter rating and he asked a more experience pilot about the trouble he was having and the pilot told him to look up and after consideration from the less experience pilot that worked for him, so look up at what-- the rotor, something at eye level or not to look at the ground. What I am trying to determine here is how to hover a helicopter, what control inputs do you have to make and in what order, I have heard that once one control input is made you have to use all of the controls but dont you have to do it in a certain order and where and what are your eyes focused and what are the cues that you are looking for to determine which control input is needed. I am trying to determine the mechanics and the cues needed to hover. Thanks in advance for your response. |
#6
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Here is an excerpt from a previous posting here, author unknown but
knowledgeable. While he/she doesn't specificly address the "hover" alone an explanation can be derived from it; ? O.K. Here we go! As soon as we get off the ground we notice a tendency for the helicopter to drift to the right due to the tail-rotor's thrust, so a little left cyclic *pressure* is necessary to stay over one spot. I say pressure because that's all it takes. Much more than that and the helicopter will go too far to the left and slip off the "cushion" of high-pressure air it is producing under the rotor and will settle to the ground if power is not added. Not only that, but a series of pilot-induced oscillations on all axes may develop. Let's say that we move the cyclic to the left to correct for tail-rotor drift, and have to suddenly move it back to the right to correct for the over-correction. Now we find ourselves swinging back and forth to an increasing and alarming extent. This is due to the helicopter's mass acting as a pendulum under the spinning rotor, which tends to stay put much like a spinning top. This is appropriately called "pendular effect". Not to over-complicate things, but pendular effect is not the worst thing to deal with when in a hover. Let's say that we experience tail-rotor drift and correct for it using left cyclic pressure. Although the rotor is still producing the same amount of thrust, we have just converted some of that lifting thrust (called "lift component") to lateral thrust ("thrust component") by tilting the rotor disc slightly. To avoid settling to the ground, we must add some lift component by adding collective and simultaneously adding enough throttle to maintain rotor RPM. While doing that we notice that the nose of the helicopter wants to go to the right due to the increase in torque, so we add some left pedal pressure, which stops the nose from moving, but since the tail rotor needed more power to do that, and it doesn't have its own engine, we had to steal some power from the main rotor. (Ya faller me?) Now that the rotor has less power, the helicopter wants to settle to the ground again, so we need to add more collective and more throttle and more pedal... now you're too high! Uh oh! Less collective! Less power! Right pedal! Now you're drifting to the left due to less thrust from the tail rotor! Watch that rotor RPM! Better get outa this hover and away from the ground where its safe! Now here's the fun part. Gently feed forward cyclic pressure and simultaneous collective/throttle (and don't forget left pedal) until we begin to gain forward speed. Now we just lost two good things: Ground effect, which is that cushion I mentioned, and lift component since we tilted the rotor forward. Just add some collective/throttle to keep from digging a hole, and the appropriate amount of pedal to hold heading. We quickly gain forward speed until we gain a good thing to replace the two good things we just lost: translational lift. Translational lift is what people are referring to when they say that a helicopter's rotor system acts like a wing in forward flight. Kinda sorta, but not exactly. It *flies* much the same but not because of wing-like properties. It is simply because the helicopter now has a constant supply of "still" air to climb upon, rather than sitting in its own accelerated column of air. We can either choose to nose over a bit more or reduce power and stay near the ground to accelerate some more, or let the helicopter climb with its newfound extra rotor efficiency--its your choice. (O.K., we skimmed the ground 'cause its fun.) Now we need to get over those trees...c'mon, that's enough! Now, ease back on the cyclic enough to maintain good climb speed and up we go like that Ferris wheel you used to hate so much. The easiest part of all needs little explanation. Just do all the same stuff you do in an airplane plus watch your rotor RPM. When you want to turn, give it a little pedal to coordinate. Hold speed by holding *attitude* with the cyclic, hold altitude with the collective. Easy, huh? There's a little more to it, but you might not notice it while in flight. Some things change with speed, and some mostly sub-conscious corrections need to be made, but there are limits to sub-conscious flight techniques. The following paragraph is optional reading for those who only want a very basic explanation of helicopter flight. (this involves math) :-) Due to the rotor spinning rapidly, and the helicopter as a whole moving forward, we have to deal with "dissymmetry of lift". Dissymmetry of lift comes from one side of the rotating rotor disc moving into the direction of travel of the helicopter, and the other side moving away from it. The net effect is to add the speed of the helicopter to the rotor's rotational speed on the dvancing side, and conversely to subtract the forward speed of the helicopter from the retreating side of the rotor. If the rotor has a rotational speed of 400 MPH at the tips, and the helicopter is traveling at 100 MPH through the air, the net speed of the advancing side of the rotor is 500 MPH. Under the same conditions, the net speed of the retreating side is 300 MPH. If an airplane tried to run its right wing through the air at 500 MPH and run its left wing through the air at 300 MPH, it would be doing snap-rolls until it crashed. Dissymmetry of lift is the primary obstacle the helicopter faces in significantly improving on current top speed records. Above the approved top speed of a helicopter, the rotor blades are alternately experiencing the extremes of Mach buffet, and of reverse flow...450 times a minute. The resulting rapid oscillation of center of pressure on each blade can lead to catastrophic rotor system failure. The vibration is a warning. The control effect as speed increases is that the helicopter rolls towards the retreating side, and is corrected by adjusting cyclic pressure against the roll. This is done without much thinking except to re-trim the cyclic when speed changes significantly. Another change that isn't really noticed is that the tail-rotor doesn't need to work as hard at higher speeds due to the weather vane effect of the tail boom. Airfoils are often placed on the boom to unload the tail-rotor at high speed/high power settings and free up power for lift/thrust. This is boring as hell, so now we're going to land somewhere...anywhere. See any place you want to stop and have a picnic? How 'bout that little pond with the ducks and the waterfall tucked into that gorge? Let's land on that sand bar. This is one place where those fixed-wingers won't bother us. Losing speed and altitude is basically the reverse process of gaining them. To hold altitude and lose speed you ease back on the cyclic to flare and reduce speed while lowering collective/throttle just enough to hold altitude and maintain rotor RPM. To lose altitude without losing speed, lower collective/throttle until the desired rate of decent is reached. A combination of both is usually used for approach to landing. At the point of loss of translational lift, the rotor system will vibrate a bit, but you're used to it by now (you'll be a bit numb by the end of the flight). Besides, you'll be somewhat distracted by the sinking feeling, followed by the confusion of having the nose suddenly jerk to the right when you yank up on the collective to stop sinking. (forgot that left pedal again, eh?) Anyway, when you've established a hover (hopefully in ground effect and over a clean, level spot) you can decrease collective until touching the ground. That was an over-simplification, but you get the idea. Now we can eat. Don't freak out too badly when you notice those wires--damn close, but you're alive! "Wannafly" wrote in message oups.com... Hello, what are the control inputs required in a hover in an ideal situation, what I am trying to figure out is what are you doing in a no-wind situation to hover. |
#8
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