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Questions tagged [control-surfaces]

Use for control surfaces; for the cockpit controls, use [flight-controls] instead.

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Acceleration command in proportional navigation?

I was recently taking a gander at proportional navigation, a missile guidance law, and I noticed most PN laws output something known as an acceleration command. The acceleration command is a command ...
KING MOOSE's user avatar
2 votes
1 answer
68 views

Why does forward CG decrease controllability/maneuvarability?

Why is a larger elevator input required to change the pitch of an aircraft with a more forward CG? I would think intuitively that the farther forward the CG, the greater the arm between the elevator ...
Terry's user avatar
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0 votes
1 answer
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Can a single-bladed rotor with cyclically varying torque emulate a swashplate?

Instead of a swash-plate cyclically varying the pitch of the rotor blade(s), could a similar effect be generated by cyclically varying the thrust of the motor on a fixed-pitch single-blade rotor? The ...
Albeit's user avatar
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4 votes
2 answers
341 views

Are control surfaces less effective at supersonic speeds?

I am unsure if this is correct but this is my current explanation: Once past supersonic speeds, the larger the speed the larger the divot of air pressure around the plane. Because these divots can get ...
Sam Jones's user avatar
2 votes
1 answer
242 views

How to develop motion model for RC plane

I'm interested in controlling an RC plane autonomously, and to do that I need a basic motion model. How would I do this? Particularly without a wind tunnel?
FourierFlux's user avatar
12 votes
5 answers
4k views

Why isn't the rudder below the tail?

Most airplanes have a rudder on top of the tail. When it is turned to the left, it causes the plane to yaw to the left. But it also puts a roll force to the right, because it is usually above the ...
Lycodo's user avatar
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1 vote
1 answer
500 views

How are flaps and the elevator positioned in cruise?

so I understand that an elevator is used to maintain cruise (straight level and unaccelerated flight) but I’m curious now about how the flaps and elevator is positioned whilst an aeroplane is trying ...
James's user avatar
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2 votes
0 answers
205 views

Boeing 777 PCU Synchronization of Duplicate Hydraulic Actuators for Control Surface Deflection

I have a question regarding the redundancy of hydraulic systems used to deflect the control surfaces of a Boeing 777 aircraft (or the like). We know that "the elevators, ailerons, and flaperons ...
Adam Yassine's user avatar
5 votes
1 answer
488 views

How do rolling airframe missiles steer?

There are a certain type of missiles that roll constantly in flight, so-called rolling airframe missiles. Missiles found in the category range from various MANPADs, to the creatively named RIM-116 ...
PeriodicParticle's user avatar
4 votes
2 answers
2k views

Why does the trailing edge have a more pronounced taper than the leading edge on the Cessna 172?

Why does the Cessna 172 have a more pronounced taper on the trailing edge as opposed to the leading edge?
Boeing787's user avatar
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19 votes
0 answers
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What causes the "dead band" phenomenon during takeoff on the Boeing 737?

During takeoff, the Boeing 737 encounters a distinctive "dead band" phenomenon after the initial pitch reaches approximately 10 degrees. Essentially, a slight increase in back pressure is ...
tedioustortoise's user avatar
4 votes
1 answer
170 views

Are flaps regulated as balanced control surfaces?

I was talking about flutter the other day and how it occurs with the ailerons able to flap out of sync with the wing. I realized that the flaps, could in theory, move in a similar way. However, the ...
Kenn Sebesta's user avatar
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0 votes
1 answer
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How do hybrid control surfaces work?

I am trying to build a self-stabilized model rocket with actuated fins. Suppose the rocket has 4 fins. The diagonal fins must rotate together to control the yaw/pitch motion, and all the fins are ...
Leo Liu's user avatar
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1 vote
1 answer
146 views

Control surfaces on radio-control models of airliners

Do large RC airliners like the huge Emirates RC A380 still need all the same control surfaces that a real A380 has I,e leading edge slats? If not why is this the case. Many thanks for your time in ...
Lee's user avatar
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23 votes
4 answers
4k views

Why were the Space Shuttle's elevons reversed, early in re-entry?

The veteran Space Shuttle commander Charlie Precourt writes, in the July 2022 issue of EAA's Sport Aviation, p. 38: Another interesting reality about our flight controls was their working essentially ...
Camille Goudeseune's user avatar
3 votes
2 answers
769 views

Are spoilers primary or secondary flight control surfaces?

The literature on primary and secondary flight controls is very contradictory. My professor provided this image from which I infer that spoilers are used for primary flight control: Also, here it ...
Yaso's user avatar
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5 votes
3 answers
1k views

Could a trim system conceivably manipulate only primary surfaces?

Most airplanes' trim systems manipulate a tab associated with a primary surface. For example, a pitch trim tab (secondary surface) is attached to the elevators (primary surface) and will change the ...
Charles Nicholson's user avatar
-8 votes
2 answers
194 views

What about measuring airspeed from control surface forces on the framework?

I watch a lot of these videos that people make about air disasters. One factor that seems (or hopefully seemed) to crop up is where pilots get hopelessly confused about airspeed, particularly (it ...
mike rodent's user avatar
13 votes
3 answers
2k views

Why are the red/white control surfaces under the wing extended during a take off?

These pictures are more than a little dated as the CF-101 Voodoo's have not been flown since the mid 80's. In these two photos we can see the Voodoo is performing a full afterburner take off. Note ...
Forward Ed's user avatar
-2 votes
2 answers
198 views

How does control system design ensure correct elevator position with the steering system unlocked? [closed]

I’m having some trouble answering the following problem encountered in one of the worksheets for aviation students: The plane shown in the picture stands on the runway. The pilot, while getting off, ...
EngineerInProgress's user avatar
0 votes
0 answers
120 views

what is considered a good pedal performance in a fighter?

What is considered a good performance in designing the directional control law in a fighter? Is it acceptable to have some roll when using a pedal? For example, is it acceptable to have 40 degrees ...
jenifer's user avatar
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2 votes
1 answer
176 views

Does the pilot always need to use stick to compensate roll caused by pedal?

When the pilot uses pedal in a fighter like F-18, does the aircraft roll? If so, is it the pilot's job to compensate this roll or the control system compensates it automatically? In other words, is it ...
jenifer's user avatar
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0 votes
1 answer
189 views

Control surface deflection during takeoff

What is a reasonable (or typical) control surface deflections required for takeoff? I would like to know two ball park values if possible elevator deflection for conventional transport aircraft ...
Omar Khammash's user avatar
6 votes
2 answers
2k views

Why are there no high wing Canard airplanes?

Just had a thought about canard airplanes while looking at the Tu-144 that features a canard surface on the top of its fuselage. Are there any high-wing aircraft with a top or bottom mounted canard? ...
Gerry's user avatar
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13 votes
1 answer
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How are control surface problems in wings having high bending dealt with?

In some aircraft which have large wing deflection due to bending, do ailerons or flaps not get stuck or bent themselves? In the case where hinging axis is also bent how do ailerons operate?
Mridul's user avatar
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11 votes
2 answers
2k views

How exactly do the Beechcraft 1900's stabilons work?

The Beechcraft 1900, in addition to the usual wings and vertical and horizontal stabilizers, and the extra vertical tail surfaces added for improved directional stability, has a pair of horizontal ...
Vikki's user avatar
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4 votes
1 answer
400 views

What is the maximum control surfaces deflection on a Cessna 210N?

Does someone know how far the control surfaces (rudder, ailerons, elevator and nose gear) can deflect in a Cessna 210N? I've been searching Google and the POH for hours now and can't find it.
TheEagle's user avatar
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2 votes
1 answer
710 views

Why would control-surface balance horns cause problems at transonic speeds?

On many aircraft, control surfaces such as elevators, ailerons, rudders, etc., have "horns" which extend forwards of the surface's hingeline, wrapping around the tip of the wing or ...
Vikki's user avatar
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2 votes
1 answer
1k views

Do the different spoilers on an A321 extend by different amounts? [duplicate]

I recently flew with an A321 and watched the left wing while the pilot tested the control surfaces before lift off. I noticed that one of the spoilers angled upwards much less than all others. In the ...
Daniel Sk's user avatar
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15 votes
2 answers
4k views

Why are the grid fins on Starship pointy and sharp?

The grid fins on Starship are serrated, why? Does it help in transonic maneuvers? Source: Starbase Factory Tour with Elon Musk [Part 1], YouTube, at 30:28
Pioneer's user avatar
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3 votes
1 answer
158 views

Angle of Attack influence on Adverse Yaw

we are analyzing an aircraft's lateral-directional control characteristics with self-made code. We have observed that the aileron's influence on the body axis yaw moment is quite sensitive to the ...
rubemnobre's user avatar
1 vote
1 answer
198 views

What are the degree markers on the tail of this MD-10 for? [duplicate]

I took this picture of of Orbis's McDonnell Douglas MD-10-30. Tail: N330AU. What purpose do the 0 and 2 degree markers serve?
TayE's user avatar
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1 vote
3 answers
226 views

Replacing cyclical control with tilt-able rotor using EV motors and servos

I understand the traditional reasons for cyclical control (with swash plates) on helicopters; ie, avoid gyro effect, shaft can be fixed. However, if the power plant was a modern EV motor, and ...
Steve Clancy's user avatar
-1 votes
3 answers
288 views

What should a pilot do if none of the control surfaces are responding? [closed]

What would a pilot do if none of the control surfaces are responding? For example, a pilot flies a medium-sized plane and to make the situation a bit less hectic, they're the only one onboard. Then ...
Ginger's user avatar
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0 votes
2 answers
180 views

What suits best for lateral controllability at high Angle of Attacks- a vortex generator or wing slots?

At high angle of attacks, the prominent problem is the separation of airflow. And if this airflow separation is near ailerons, we lose lateral controllability. And the solution is making the flow ...
Noorul Quamar's user avatar
4 votes
1 answer
875 views

Why does the Cessna 208 Amphibian have extra tail surfaces?

Mark Harkin, CC BY 2.0, via Wikimedia Commons I've seen extra tail surfaces that look like additional vertical stabilizers on the C208 Amphibian. Why is there a need for this? I can't imagine that ...
MD88Fan's user avatar
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9 votes
4 answers
3k views

Under what circumstances does the F-16 and possibly similar fighters deploy leading edge slats?

What does the F-16 (perhaps other fighters as well) use to decide when to deploy leading edge flaps? I would assume angle of attack, airspeed, stick deflection, or some combination of the three, are ...
MD88Fan's user avatar
  • 2,500
2 votes
1 answer
502 views

Do the stabilators on the F/A-18 also have a roll function similar to the F-22?

I'm curious about the F/A-18C. I know it has ailerons, but they seem too small to be greatly effective at low speeds. Do the stabilators have a roll function as well? If so, is there a speed at which ...
MD88Fan's user avatar
  • 2,500
9 votes
6 answers
2k views

Can flaps be used to perform rotation and flare?

TL; DR using flaps to directly control sink/climb rate near ground = simpler and faster response = easy to fly airplane? Rotating is the pitch up during takeoff that causes the aircraft to leave the ...
Abdullah is not an Amalekite's user avatar
0 votes
0 answers
264 views

What are typical control surface deflection "rate" limits for transport airplanes?

I was wondering if anyone knows what are some typical control surface/actuator deflection "rate" limits for transport airplanes (i.e. aileron/elevator/rudder deflection rates)? I haven't ...
Chuy's user avatar
  • 1
0 votes
1 answer
171 views

What does gravity compensation do in flight control?

In flight control designs for lateral directional movement, there is a block named "gravity compensation". This block changes yaw rate measurement from "$r$" to "$r-g/Vcos(\...
shooshool's user avatar
  • 407
11 votes
3 answers
3k views

Why do the ailerons of this flying wing work oppositely compared to those of an airplane?

I made this simple wing glider and put some ailerons on it. I thought that the ailerons in this glider would work the same way it works on airplanes, wherein the roll will be in the direction of the ...
Adriel Mattheuz Estolano's user avatar
5 votes
1 answer
2k views

How do tailless aircraft yaw? [duplicate]

I was doing research on control surfaces present on an aircraft and I noticed that some aircraft like the B2 Spirit does not have a vertical tail stabilizer and therefore no rudder either. How do ...
Synchronicity's user avatar
9 votes
1 answer
1k views

In missiles, what actuators are used for the control surfaces?

In a normal airplane, hydraulics or even cable-pulled systems are used to power the control surfaces. In a missile, that seems infeasible. What device is used to move the control surfaces, and where ...
DrZ214's user avatar
  • 17.9k
5 votes
2 answers
950 views

What, if any, would be the most correct term for the aerodynamic flight control surfaces of SpaceX's Starship?

SpaceX's Starship uses a unique flight control scheme during descent that I have not seen anywhere except with skydivers: it falls straight down belly-first using four aerodynamic control surfaces at ...
Jörg W Mittag's user avatar
6 votes
2 answers
2k views

What is the benefit of a horn control surface?

Like the one above. Is it just so that you can hinge closer to the leading edge of the aileron or control surface? Why did the designers of the ATR-72 elect to use this feature?
Rory McDonald's user avatar
1 vote
2 answers
400 views

How do fighter jets stop pitching motion after a elevator deflection?

I'm working on a flight simulator , In which the jet has only ailerons , rudder , and two elvators at the back . When I nose up my aircraft via elevator deflection , it just keeps pitching up ( even ...
GopalSir's user avatar
0 votes
2 answers
199 views

What control surfaces do I need to move to do a roll in a model aircraft?

Figured that this was the better site to ask than drone SE, but if I'm wrong just let me know. I'm making a spitfire model and was just wondering how do I do a roll? I have elevator, rudder, and two ...
Ceramicmrno0b's user avatar
0 votes
2 answers
712 views

On large aircraft, why do flaperons not run the full length?

This is a 777 flaperon. It looks rather tiny, compared to the flap. There have been air disasters where the airplane rolled uncontrollably for one reason or the other. It seems to me that a larger ...
Abdullah is not an Amalekite's user avatar
0 votes
2 answers
127 views

What is the name of Control equipment? [closed]

I wanted to know the name of equipment that controls the control surfaces of an aircraft by taking commands from the pilot through it's hotas stick. The aircraft could be a combat 50's or 60's a/c, so ...
scico111's user avatar
  • 155