![]() |
If this is your first visit, be sure to check out the FAQ by clicking the link above. You may have to register before you can post: click the register link above to proceed. To start viewing messages, select the forum that you want to visit from the selection below. |
|
|
Thread Tools | Display Modes |
#131
|
|||
|
|||
![]() "Mxsmanic" wrote in message ... writes: You're demonstrating that you've never been in a real plane, nor even in a good simulator ("good" meaning one that simulates control pressure). Some people here have only been in one type of aircraft, and mistakenly believe that all aircraft are the same. Anyway, if you're trimmed for a very slow airspeed, (high AoA, nose-up pitch) you'll absolutely know it. You'll know it by the sloppy feel of the controls, the sound the plane makes, and your airspeed indicator. Likewise, if you're trimmed for a very high airspeed, you'll know it by the stiff controls, the sound, and the airspeed indicator. In some aircraft, yes. But I wouldn't trust that in all aircraft. How would you know, you can find your fat ass with both hands just reading the regs. |
#132
|
|||
|
|||
![]() "Mxsmanic" wrote ... Well, you really go to great lengths to demonstrate your stupidity. I wonder why? Let me recall the context of my question, which you cut out: There are several ways to implement an autopilot. But no autopilot is designed to relieve control pressures. What do you think this one does? "The FCCs also operate together to provide the automatic pitch trim function. The FCCs sense torque on the primary pitch servo and generate arm and command signals to drive the pitch trim servo or external trim control system." Then you answer with: It maintains altitude. Your answer is a) out of context, b) erroneous, being seriously incomplete, c) demonstrates an attitude of trying to use convenient part-truths to argument your viewpoint even when it has already lost. A not unknown debating tactic, but useless nevertheless. |
#133
|
|||
|
|||
![]() |
#134
|
|||
|
|||
![]()
In rec.aviation.piloting Just go look it up! wrote:
On Sat, 14 Apr 2007 16:25:02 GMT, wrote: In rec.aviation.piloting Mxsmanic wrote: Snowbird writes: I can see you have actually begun to learn something about autopilots. There is more to the story, though. Would you believe some autopilots act on both the control surface and the trim device? There are several ways to implement an autopilot. But no autopilot is designed to relieve control pressures. Another true but worthless statement. Hmm... Is it a true statement though? The King autopilots (and the S-Tec range AFAIK) both are designed such that they use pitch servos to reposition the control surface (elevator or stabilator) to affect a change (climb, descent) and have inbuilt feedback generators to tell the trim servo to actuate such that it removes the load from the surface at its new position. That seems to be at least two systems who's basic design incorporates a methodology to actively relieve control pressures. You are being realistic and practical in your interpretation. He is being a pendantic, semantic game playing, asshole in he's interpretation. Strictly, he is correct. Autopilots are designed to control aircraft. -- Jim Pennino Remove .spam.sux to reply. |
#136
|
|||
|
|||
![]()
Just go look it up! wrote:
design goal of an autopilot system, and he switches back and forth to suit whichever asinine argument he's proffering at the moment..... And everybody sucks it up like a sponge, responding to the troll just like he wants.... |
#137
|
|||
|
|||
![]()
Just go look it up! writes:
Hmm... Is it a true statement though? The King autopilots (and the S-Tec range AFAIK) both are designed such that they use pitch servos to reposition the control surface (elevator or stabilator) to affect a change (climb, descent) and have inbuilt feedback generators to tell the trim servo to actuate such that it removes the load from the surface at its new position. That seems to be at least two systems who's basic design incorporates a methodology to actively relieve control pressures. Relieving control pressure is still not the purpose of the autopilot, though. It merely uses that as a means to an end. If autopilots were really intended to relieve control pressures, then they would not hold altitude or heading. Instead, they would act to keep the controls in whatever position you last put them in, irrespective of altitude or heading. I don't know of any autopilot that does that. The closest approach is the control-wheel steering feature of some AFDS systems on large transport aircraft, but apparently pilots don't use those features very often, and it's still based on maintaining something other than control pressures. -- Transpose mxsmanic and gmail to reach me by e-mail. |
#138
|
|||
|
|||
![]()
Mxsmanic wrote in
: Snowbird writes: Autopilots certainly want to trim out control pressure. Think about what would otherwise happen when you disconnect the autopilot. Duh. It actually _does_ happen when you disconnect the autopilot, in some aircraft. The purpose of the autopilot is not to relieve control pressure, it is to fly the aircraft. In aircraft that use trim for the autopilot, the aircraft may be stable when you turn the autopilot off. However, in aircraft that directly manipulate the controls with the autopilot, the aircraft may suddenly change attitude when the AP is shut off, if the AP has been compensating for something (such as an engine failure) while it has been operating. This has caused accidents. You have no idea what you're talking about, fjukktard. Bertie |
#139
|
|||
|
|||
![]()
Mxsmanic wrote in
: writes: All real aircraft have elevator trim. Not true. Some move the stabilizer instead. That's stil trim, you moron. Berti e |
#140
|
|||
|
|||
![]()
Mxsmanic wrote in
: writes: Assuming you're in straight and level flight, with constant power setting: when you change trim, do you adjust the yoke (or joystick) position to keep things straight and level? Only if the trim adjustment puts me out of trim. Then I have to hold the yoke continuously. If I gradually trim correctly, I can apply less and less pressure to the yoke. You can't do any of the above. You can't fly. Bertie |
Thread Tools | |
Display Modes | |
|
|
![]() |
||||
Thread | Thread Starter | Forum | Replies | Last Post |
Methods of launch | Jim Culp | Soaring | 0 | November 20th 06 07:39 AM |
Methods of Launch | Nigel Baker | Soaring | 3 | November 17th 06 04:35 PM |
methods of lauch | Robert Gaines | Soaring | 0 | November 16th 06 01:17 AM |
Vector altitude for ILS below GS intercept altitude? | M | Instrument Flight Rules | 23 | May 20th 06 07:41 PM |
Pressure Altitude or Density Altitude | john smith | Piloting | 3 | July 22nd 04 10:48 AM |