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Last Updated on Tuesday, 24 June 2008 08:37
 
The 2 DOF Helicopter

 

MEM Undergraduate Honors Research Program:
2 DOF Helicopter
Timeline: 1/2005 - 3/2005

Page Last Updated: 2/16/2005 9:55 PM [FINAL UPDATE]

 

 

Project Abstract

      I will work with Dr. Oh this term to develop a Two Degree of Freedom (2 DOF) Laboratory Helicopter. This device would be used for demonstration and mechanical engineering laboratory classes. It would be used to study aerodynamics, fluid mechanics, nonlinear control, and more. It could also be used as a platform for more advanced experiments. The device already exists and is available from a supplier (Quanser), but the high cost is prohibitive for most environments. The goal of this project is to develop the highest quality version of the device which could be produced for a more reasonable $500-$600. We may share this plan with the academic community by publishing a paper in a scholarly journal. I will be concerned mainly with the mechanics of the device, and a basic control system. The control system will be further developed by a group with appropriate expertise.



2 DOF Helicopter Design Example

Picture Source: www.quanser.com      



      The  helicopter itself is comprised of a central column, about which an arm can rotate. The placement of airfoils is identical to many real-world helicopters: one on the top front for lift, and one on the tail to compensate for the torque effect produced by the main airfoil. The  helicopter will be able to pitch and yaw by manipulating the two airfoils. This device presents several design challenges, including an electronics system with components that can rotate indefinitely. (See Figure 1). We are in no way reverse engineering Quanser's device, as we do not have one of their models. They have made a description, pictures, and movies of its operation publicly available though. See their version here.

Dr. Oh is the Project Advisor. We have developed this abstract together, and plan to adhere to the schedule below. I will consult him or his Graduate Students for any problems, and meet with him regularly to discuss progress and re-assess goals. I will spend approximately 6-8 hours per week on the project, not including a weekly program meeting and a weekly advisor meeting. Throughout, I will create and maintain a web-page logging the development of the project. My final deliverable will be a formal 20-minute presentation. Please note that the timeline and deliverables of the project have been modified with Dr. Oh's guidance throughout the course of the project.



Work Log

 
Date Activity                                                                                                                                                                                                        
1/17/05 Optical Encoders
1/20/05 The Slip Ring, Part 1
1/22/05 The Slip Ring, Part 2
1/29/05 Design, Part 1
2/22/05 It's Alive!
4/16/05 Final Presentation and Future Work



1-17-05: Optical Encoders  
      To build this helicopter we will need a way to control it, and see what it's doing. Sensors will allow us to do just that. One application would be to see how far the center column has spun, which is the yaw of the helicopter. It would also be nice to see how fast it is spinning (the angular velocity) and how that spinning is changing with time (the angular acceleration). For my project, I will create a simple open-loop control system. That means that the sensors will only be read to see what the helicopter is doing. Later, a closed-loop system could control the helicopter using input from the sensors.     


Source: http://fargo.itp.tsoa.nyu.edu/~ms1436/sensors/optical.html

 


      What is an optical encoder? Basically, it's a spinning disk with holes in it. (It gets more complicated, don't worry.) One one side of the disk is a light source. On the other is a light detector directly across from the source. As the disk spins, the detector can see the light when there is a hole, and can't see it when there is a solid part. Thus, the signal will go on and off (digitally) as the disk turns. What good is a disk with holes in it though? To make it useful, a shaft is connected to it. That shaft can then be coupled to just about any rotating system. By recording how many times the signal goes on and off, we can tell how far the shaft has rotated. By recording the time of each "off" signal, we could find the angular velocity. More interesting things come from that point on. Note that some mechanism is also present to tell which direction it is turning in. This is most likely in the form of a second set of holes, purposely offset. Mechanical encoders are also available. They would do something like depress a switch as a gear ridge passed. They lend themselves to slow, simple movement though. Thus, an optical encoder with its capability of high speeds and accuracy lends itself to this application. Note that encoders only give a relative position, not an absolute one. It would have to be calibrated and "zeroed" to give a useful position. Slippage would be a major problem, because the software and hardware would then be out of synchronization. [My HTML editor didn't remind me to save any of the above "Optical Encoders" section so it was all lost and re-done...I must find a new HTML editor.]
      I experimented with a US Digital Optical Encoder and "Encoder Data Acquisition USB Device" called the "USB1-S." To experiment with it, I drew a circle and marked its degrees with drafting tools. Yes, the pointer that I attached really is a binder clip and a post-it note. Hey, it worked. (See below)

 



         

 

After calling the company to get the drivers for the device, I was able to connect it to my PC via USB. This is a convenient alternative to a DAQ (Data acquisition Card). Basically, it allowed the signals from the encoder to be sent to my computer for processing. The program that they included works on a basic level as is. It allows you to see a diagram and associated numbers as you turn the shaft for up to 4 encoders. The manual included a good deal of programming and electronics instructions, which are beyond my understanding. Some features are:

  • logging what happens to a file, either continuously or only when something moves
  • Triggering other programs when a certain event occurs (Such as Encoder #2 moving more than 90 degrees, or traveling 10000 rotations)
  • Variable Resolution (More on that soon)
  • Multiple Counting Modes

       The manual and full features of the hardware and software can be found here: http://www.usdigital.com/products/usb1/

 

            

 

On the left is a picture of the main program screen. Note the time stamp on the left, which is continuously counting in microseconds. The hardware can accept up to 4 encoder inputs, so 4 are displayed on the screen. Notice on the right that values have been changed for all 4. To do this I simply plugged the one encoder that I had into each port separately. The software could do 4 simultaneously though. 
      I then began to do some quantitative experimentation. I first noticed that the dial on the screen moved in the opposite direction to my pointer setup. It would match if my setup were upside-down. I tried to find a way to reverse it, but did not. I'm sure with some clever programming it would not be a problem. The basic interface for each encoder allows you to name the encoder, see the position, adjust the resolution, change the counting mode, and reset the position to zero. The resolution didn't do what I thought it would at first. I expected the software to see 1 full rotation every time I did one on the encoder. I then expected the resolution to break up that rotation into smaller pieces as I increased the resolution. After checking here, I now know that the resolution actually changes the number of pulses per revolution. That's how many times the encoder says that it hit a solid point per revolution. The disk inside must be very precise, because the resolution goes up to several thousand. I played with the resolution until I could get the software to match the rotation of the encoder. It works best at 980 as far as I can tell, so I imagine that the number of openings on the disk is around 980. The counting mode (1x, 2x, 4x) seems to just multiply the movement of the encoder by that number. For example, after I calibrated the resolution to 980, I changed the counting mode. At 2x, the software turned 180 degrees when I turned 90. At 4x, it made a complete circle. I also noticed that every time I moved the encoder, a green LED marked "activity" lit up on the box next to the encoder input.
      This system offers a great deal of possibilities. With some programming, it could be very useful for my application and many others. The USB-1 device costs $300 though, and is rather large. It's also overkill for what I want to do, so I know we will have to use some other device to interface with the computer. This will probably be in LabVIEW, which is also provided by US Digital. We'll eventually use a DAQ of some sort to simplify the operation and lower the cost significantly.

[Setting up the website and creating this section took about 7 hours rather than the 3 that I had scheduled for it. Hopefully it'll go smoother from here on.]




1-20-05: The Slip Ring, Part 1  
    A crucial part of the design of this helicopter is the slip ring. What is a slip ring? It's a device that allows electrical connections to rotate indefinitely, without any wires getting tangled or wound up. Sounds like just what we need for the yaw (rotating around the center column) of the helicopter. First of all, the links below have nice explanations of how slip rings work:

How slip rings work:  Berton.com.sg

                                 uea-inc.com  (FLASH Animation)
                                 sliprings.com

Note that there are also alternatives to the traditional slip ring, such as Rotating Electrical Controllers (RECs). For now, I will focus on slip rings. They are a tried and true technology, will serve our purpose, have many suppliers, and that's what Quanser used. On another note, it appears that building a slipring of sufficient quality from scratch in this time would be impossible. It would have to come in the form of a stackable kit or something similar. So far, I have been unable to find any such thing. It looks like we ll have to buy it, hopefully at a reasonable price. If the prices look too high though, I'll certainly try to learn how to fabricate one. Now to make it practical for this project, we need to know how it will be used in the helicopter. First we need a layout, so we'll start with the one from Quanser. (Top of Page) My design drawing is soon to come, even if it's hand-drawn. For now, I have assembled a parts list:


Parts List


Electronics: 

Slipring (low friction) - Need to Finalize number of "channels"                                        

Optical Encoder for yaw (z-axis)
Optical Encoder for Pitch (mounted with some mechanical cleverness)
Computer Interface / Board
Control Device (Joystick?)

Power Supply (DC)
Mechanical: Main Airfoil (Enclosed)
Tail Airfoil (Enclosed)
Main Motor (DC)
Tail Motor (DC)
Base: Stand/Base

Helicopter Frame

Mounting hardware (screws, etc.)

    
From the above design, it seems we will need five channels in the slipring:

Slip Ring Channels

Type (I/O)

 Channel            

Input Optical Encoder for Yaw
Optical Encoder for Pitch  (mounted with some mechanical cleverness)
Output Main Motor
Tail Motor
--- Ground



 

 

 

 

 

 

 

 Quanser used an 8-Channel slipring, and uses this phrase in the product description: "The coupling between the pitch and yaw motor torques results in a coupled 2 input - 2 output system. I will have to consult Dr. Oh for further guidance on these points. As for the suppliers, I have compiled the following preliminary list:

 

Potential Slip Ring Suppliers (Not a final list of course)

http://www.rotarysystems.com/
http://www.mercotac.com/ (alternative to slipring)
http://www.uea-inc.com/slip/index.html
http://www.polysci.com/SlipRingcatalogsummary.htm
http://www.smallparts.com  (website down when I tried it)
http://www.grainger.com
http://www.mcmaster.com/ (NONE?)
http://www.robotcombat.com/links-suppliers.html

More to come soon.




1-22-05: The Slip Ring, Part 2  
I have come across a few more potential suppliers. Here is an updated list of suppliers, in order of their potential (Best to worst):

Rank Company (Click for link) Comments
1 Electro-Tek Looks most promising at this point, with its H series. That model is designed specifically to be small and inexpensive, for applications such as robotics. Sounds just about right. The parent company is based out of the UK, so doing business with them would be interesting. I'll get a quote soon.
2 UEA-Inc This site had the nice FLASH animation. Their products seem rather large and bulky, for industrial applications. They may have smaller ones though.
3 Techtron Corporation This site looks like a small business that may be able to help us.
4 FabriCast Another small business, with some pre-designed slip rings that might work.
5 MOOG Are these the same people who made the MOOG synthesizer, or am I spelling that wrong? They require that you order a catalog to get any information, so I'll have to check with Dr. Oh about that. I'd rather we don't get onto any unnecessary mailing lists. Perhaps I'll just call to inquire.
6 Mercotac Alternative to traditional slipring. Brushless, so better longevity. Probably not a necessary improvement (or cost) for this project. Worth calling though.
7 McMater - Carr Limited selection. All models have plug style connectors rather than wires. Will go here for the slip ring only if the others don't work out.
8 Robot Combat An interesting hobby site for competitive destructive robots (battlebots I'm assuming). Lots of supplier links, but no slip rings come up on the search. May be good for other electronics though.
9 Grainger Don't carry slip rings, though a search for them on the website does return some kind of plastic pump connector thing. May use them for other parts of the helicopter.
10 Small Parts Don't carry slip rings. May use them for other items on our parts list though...
11 NASA Here's an interesting idea from the NASA Ames Research Center: We won't need something so advanced, but this is an example of the progression of rotating electrical equipment technology.
12 Rotary Systems They actually make a product for mechanical rotation, not electrical. Interesting though.

     I will certainly have to look into getting free sampls of these slip rings. In all reality, the one we choose will go in this guide with the supplier name, and may even be published. Neat. I'm also trying to utilize the K.I.S.S principle in designing the helicopter. Hopefully that works. Time to get some dollar figures on this stuff. I also need to look more deeply into the other parts of the design.


1-30-05: Design, Part 1
This week after careful consideration, I gracefully bowed out of a difficult (but very interesting) ceramics class. There just aren't enough hours in the week to do all the things I need to. Hopefully this change will help.

I made some rough sketches of the design, based on Quanser's pictures, movie, and spec sheet. These are pages 1 and 2 below. I also made some rough dynamics calculations on pages 3 and 4. Click to enlarge:

            


We had a fundamental question about the design to begin with: if the main airfoil creates a torque that's not on the axis of rotation of the arm, will it cause the arm to rotate? After some consideration and discussion, we determined that it will. I will check all of the calculations with Bill before moving forward on fabrication. I was uncertain of the dynamics equations to use, but did find one for thrust. I am still missing one key equation though: the torque created by an airfoil. I'll need this to determine the power required for the tail. Once we determine the thrust required for each, we'll be able to choose and order appropriate motors and airfoils. In the control code, they'll of course have to be linked to run the helicopter succeesfully. I did not include any friction in the calculations for two reasons: 1) I have no idea what it will be 2) It'll be much simpler to tweak the controls by experimentation rather than theoretically. Once we find friction that way, we can incorporate it into a simulator if desired. I also worked with Dr. Oh and Bill to prepare for purchasing items. The approved budget is:

  1. Slip Ring - The largest expense of the project will be the slip ring at $100-$125. I am planning to go with an Electro-Tek H-Series slip ring, unless FabriCast  can offer a better deal, perhaps on a more robust slip ring. They’re on PST, so I’ll call today (Friday) when they’re open.

Estimated Cost: $100-$125

 

  1. Supplies for the base and various hardware – I plan to build the body of the helicopter out of balsa, per your suggestion Dr. Oh. The base could probably be made of something denser, hopefully a machinable plastic, metal, or harder wood. The vertical supports could be of several materials, including metal rods or wooden dowels. All of these things I expect I could find at a hobby store, unless your group has a supplier for such things. Bill, please let me know how I should go about searching for / purchasing these items.

Estimated Cost: $50

 

  1. Motors/Airfoils – Still remain to be discussed specifically. After some rough calculations which I will check with someone soon, it appears that the main airfoil assembly will have to produce 7.6 N of thrust. Does that value seem at least in the right order of magnitude? I am uncertain of the power requirement for the tail assembly. The Quanser airfoils had diameters of 280 mm and 203 mm for the pitch and yaw, respectively. Again, I’ll heck this with someone in the lab.

Estimated Cost: $20 (for both motors) + $40 (for both airfoils)

 

  1. Electronics - Still remain to be discussed specifically. We’ll need two optical encoders, a power supply, a board, wires, the op-amps (as you described Dr. Oh), and probably some other small things. Will we be using this with other lab equipment, or should it be stand-alone? (Especially for the power supply)

Estimated Cost: $120 (for both Encoders) + $40 (The rest)



      Total Estimate:  ((Sum of Estimated Costs) + (10% for tax and shipping)) + (10% for buffer) = $450

                                    Total Estimate: $450



I got the procedure for ordering, and the money is approved. We're good to go. Note that I will be looking into a few other sources for the slip ring before ordering: MSC, "H&R", and Electronic Goldmine.

Yesterday I was able to attend an ASME/AIAA Mini-Symposium in Plymouth Meeting. The people and presentations were very interesting, the food was good, and Congressman Curt Weldon was inspiring with his vision of a "smart region." A good experience, especially for my first technical conference. I'm sure it won't be the last.

 


2-22-05: It's Alive!

As the Work Log above may have shown, I have not updated the website in some time. I have certainly been busy on this project though. A brief summary of what has happened since the last post:

  1. Met with Mike Joyce to explore the basic theory, and get an idea of which motors and airfoils to use.
  2. Made several purchases from McMaster-Carr with the help of Bill Green to get the basic mechanical materials.
  3. Continued to work on choosing a slip ring, and got suggestion from Todd and Dr. Oh to explore using a telephone cord untangler (See one here: Phone Untangler). I have since purchased some untanglers and phone cord to test and develop for this application. The biggest barrier is that phone cords have 4 circuits and we need 6. Also, its current carrying capability may be an issue for running the motors. I'll hopefully look into this later.
  4. Continued to refine design as cleverness and/or problems arose. Discussed machining with Keith Sevcik. Dr. Oh made contact with Mark Schriber at the Drexel Machine Shop to request permission for me to use the equipment.
  5. Began making several trips to a local hardware store to get loose-end items like correctly sized washers, and angle brackets that aren't strong enough to hold up a deck (the ones from McMaster were) Also did some machining at the Machine Shop using the bandsaw and drill press. Mark and the shop staff are great guys. In out lab, cut steel angle brackets to the correct length with the masonry blade on the cop saw. Many sparks...good, safe fun.
  6. Continued putting the pieces together, refining the design, and solving problems as they arose. Got the mechanical system up and running, and made another McMaster order. Also ordered the chosen slipring, after devising a way to connect it to the optical encoder without putting any load on the slipring.
  7. Got an evaluation copy of Adobe GoLive, which I am now using to modify the webpage. I like it very much...it only supports my desire to redo this entire website in super-awesomeness. (How much of this I'll have time for remains to be seen.) An education license of Adobe Creative Suite could be a great investment. Also received 10 interviews for Co-op, and am currently working them into my schedule. Exciting in more ways than one.
  8. McMaster order and Slip Ring arrive. Put it together and....It's ALIVE as the following videos and images will show:

 

First, a brief explanation of the parts involved (more detail to follow at a later time):

 

 

  • Bases and uprights are made of HDPE, cut to size
  • Supports between bases are threaded studs, with matching press-fit inserts. This allows for solid support while allowing the system to be disassembled for repair, modification, or storage.
  • The weight of everything above the upper base rests on a simple turntable (bearings between two specially designed plates) so that the weight is not on the slip ring, as was with Quanser's design.
  • The uprights are also made of HDPE, and fastened to the angle brackets with press-fit inserts (of a different size than for the supports)
  • The helicopter body is made of balsa. It will have a nice balsa sheet fuselage for aesthetic purposes soon
  • The arm on which the body rotates is an alminum rod, which will be coupled with the encoder soon.
  • The motors were pulled from a blimp toy. Please note that they are not permanently mounted as of yet, so that I could easily modify their positions. Also note that the bolts taped to the arm served to manipulate the balance of the beam. Somethign similar but more elegant may be used in the final design.
  • The apparatus shown in the second picture above is the optical encoder for yaw. It's not connected yet, as I require an english hex key set to work with the couplings.

Below are videos of the helicopter in action. You will need the Divx Codec (click here to get it) to view them. Note that as I had one power supply at my disposal, I was only able to run one motor at a time. The function of each motor is thus showcased seperately in the videos.

 

Number
Title Caption
1 Mech. Demo The support systemin motion with the slip ring alone ( no motors or arm)
2 Mech. Demo Closeup Closeup of the above
3 Lift The lift motor operating. Note that it begins to yaw from this motor, as it should.
4 Lift Closeup (Hover) Closeup of the system with the lift motor operating
5 Yaw The lift motor operating. With some WD-40 in the turntable, friction should be less of a problem.
6 Yaw Closeup Closeup of the system with the yaw motor operating
7 Slip Ring Closeup Some good shots of the slip ring in action. The "split view" helps to understand its purpose.

 

I am excited to have gotten this far, but that's no reason to stop forging ahead. The few remaining tasks include:

  1. Permanently mount the motors / airfoils
  2. Create and mount the balsa sheet fuselage
  3. Mount the optical encoders, and mate the slipring to the turntable so that it turns exactly with it
  4. Elegance and Aesthetics: Sand, seal, and paint all of the balsa parts, tie wires down well, affix weights as needed
  5. Investigate the phone cord untangler as a replacement for the slip ring
  6. Update this website (time will determine to which extent)
  7. Create the final presentation

 

This has been quite a task so far...but I'm proud to see it working. Many thanks to Dr. Oh and his students for all of their help thus far. I could not have done much of it without your support.

 

4-16-05: Final presenation and Future Work

Here is a link to my final presentation: Final Presentation

The above presentation was given to Faculty and peers as the main deliverable of the MEM 399 class. After speaking with Dr. Oh, we determined that it would not be in the best interest of anyone involved for me to cotinue on the project independantly due to time constraints and other commitments. Instead, we expect that the completion of this project would make an excellent Senior Design Project, or could be continued by another honors student. We discussed the project in terms of Technology Readiness Levels (TRLs). You can find a link to the NASA document explaining TRL's here: Technology Readiness Levels. Dr. Oh assessed my current progress at TRL 4. He expects his Senior Design students to reach TRL 8. As such, please find two sections below giving a rough layout of how to get there.

 

The basics of the relevant TRL levels:
Click here for full NASA document. Both quotes below copied verbatim from the document linked at left.

 

TRL 4 (Current): "Component and/or breadboard validation in laboratory environment"

TRL 8 (Senior Design Goal): "Actual system completed and "flight qualified" through test and demonstration (ground or space)"

 

If I Could Have Done It All Over Again (with more time)...

  • I would first do a thorough search of the literature to. Two main purposes would be to see if anyone has already done this, and if not, to see what is available to help. Relevant writing on lab devices, sliprings, etc. would be helpful. I did do a brief search to make sure I wasn't doing a redundant project, but didn't read much. Always good to know how your work is fitting into the scientific and engineering communities.
  • I would more seriously consider building a custom slipring from scratch. This would of course be more work, especially if this project is published with recommended instructions for other academic institutions to use. The advantage would be a solid platform capable of yawing indefinitely, with an encoder mounted perfectly to it. It would also reduce friction, and ensure predictable sustainable performance. This would of course take a good deal of extra engineering to develop. The disadvantages versus using an off-the-shelf slipring would be: 1) Much more time involved 2) More difficult to reproduce 3) Possibly higher cost. I would look deeper into off-the-shelf sliprings as well, and perhaps commission a custom-made one from a company. It may be as simple for them as modifying a few drawings and making one up that does exactly what we need it to. Also, I noticed some sliprings with encoders built into them. None were the correct size for this application, but it may besomething that could be custom ordered. I also still have the Radio Shack phone Untangler, and never really looked into using that. It only has 4 conductors to be used, but someone may yet figure out a way to use it.
  • I would solve the basic dynamics equations in full. This involves some complex moments of intertia, so it may be easier to determine that value experimentally. We got as far as a few pages of calculations, and then decided to let it go. It will definitely be necesssary for writing the code though. In the world of engineering, these calculations would be relatively simple, though perhaps tedious.
  • Related tot he above point, I would figure out the exact force output and equations for the motor and airfoil system. This will definitely be required for the programming later. It would also help in choosing an appropriate motor and airfoil for the job.
  • I would use the machine shop for almost all fabrication. Often I would use the chop saw in the lab, or try to measure things very carefully with a huge T-square. Needless to say, I think my fabrication could have been a lot more precise.
  • I would order reverse-threaded (right hand / left hand) studs to use form McMaster Carr. For a few bucks this could be done even now. As it stands, I screw them fully into the bottom plate and then "unscrew" them into the top plate. They should be reverse threaded. I believe it was Mike that aptly said though, that right hand / left hand threads hardly ever work like you want them to. His idea then was to simply use a few nuts and washers to solidly connect the studs to the top plate. I agree that this would be a good approach to it.
  • I would make the airfoils look nicer. These ones were pulled right off of a blimp toy. They look okay, but nowhere near as cool as Quanser's.
  • I would MUCH more carefully do the balancing of the helicopter. Right now, there are some washers taped to the back. It works, but its precision ranks up there with trying to hang a picture frame without a level.
  • I would work on the friction problems that the device now has. For some reason, when in pitch, the two side supports seem to move closer and further away, almost as if the support bar were acting as a screw. Tried to sand it to fix it. Weeeeird though. The turntable also seems to have some "sticky" spots which silicone grease didn't make much better. What can I expect from a simple ball bearing turntable? This issue may be solved by the second bullet above though ( custom slipring)
  • I would draw the helicopter body outline in CAD, probably using a real-world helicopter as a rough template. It looks ok now, but I'm sure some CAD magic would make it look much better.
  • I would create and implement the electronics required for the system. I did not have the time or knowledge for this step, but Dr. Oh assures me that for someone with the right knowledge, it would be simple.
  • I would create and implement software to run the system. It would have a nice GUI, and would present a challenging, fun, and informative lab for the students using it. A mathematical model in MATLAB or LabView wouldn't hurt either. That way, the students could play with a "virtual copter" and then see it in the real world.
  • I would write a manual and lab to go along with the system.
  • I would test the system and refine it to get it in its best working condition.
  • I would see if the engineering education community were interested in this design and if so, write a paper for it.

 


To bring this project to TRL 8:

Please find below a rough outline of the steps and time required to bring the system to TRL 8 as an engineering design team would. Of course more may be learned throughout the re-design process that changes time requirments, or adds or removes entire steps. All hours are given in "man hours" (male or female of course) that could be split amongst multiple people. Expect that the more people are involved, a small percentage more total time would be required because of communication and the such. I imagine that for a team of 4, a 5% increase in the time required for this reason would be reasonable. I have erred on the longer side of the time estimates to reduce the chance of surprises. Please take this only as an estimate though, and change what you see fit. A 10% buffer has been added for the unknown unknowns that are bound to happen.

Step Number Step Name Details Time Estimate (Man Hours)
1 Literature Review Perform a full literature review to find sililar projects and relevant information 10-20
2 Platform design Complete the platform design. Almost all completed done, but feel free to redesign. Need some way to mount yaw encoder as well. 20-30
3 Slipring Design Could be a very lengthy process depending on the path taken. Explore: own custom design, off-the-shelf and commisioned custom design, 40-160
4 Dynamics Equations Figure out all of the equations, including the complex moment of inertia. This will be key in developing the software. An iterative process with allow the physcial design and the equations to be matched and verified. 10-20
5 Airfoil Equations Aboslutely necessary for the control and understanding the inputs and outputs of the system. Verify in the lab. 10-20
6 CAD Design [Optional] Drawing the system in CAD in 2D or 3D would be a nice bonus, and help for the precision of the system. May even be able to use this to CNC some or all of the parts! You could definitely go far (or too far) with this step. 5-60
7 Software Simulation [Optional] Create a simulation seperate from the control system. Could also integrate them (perhaps in LabVIEW) to save a lot of time. 20-40
8 Fabrication Use the machine shop! Learn the processes, and create a robust, precision product. 20-40
9 Refinement Snags are bound to come along. After fabrication, look over the design again and refine as necesary. 10-40
10 Electronics Some simple electronics are required to interface with the computer control system and perform as expected. 10-20
11 Software / Control This is a major part of the project. It involves using the equations developed before, and turning them into a real interactive intelligent control system. 40-80
12 Testing / Redesign In order to reach TRL 8, the system must be "completed and 'flight qualified' " If you expect people to use this in a lab it had better be robust and free of bugs. 40-80
13 Manual / Lab What's this great system without any instructions or guidance on how to use it? No one's going to read the manual thoroughly, so make sure your control design is free of bugs, and intuitive. I would make the lab a challenging one, as the system creates some great opportunities. 10-20
14 Presentation Of course a presentation on all of this would have to be developed and rehearsed. 20-30
15 Scholarly Paper Submission Depending on how the rest of the project goes, publishing this work as a paper may help many other institutions in creating this lab. Imagine visiting a university lab 5 years after graduation and seeing them using something they call "The Drexel 2DOF Helicopter" Even if not published in a reviewed journal, it would be an excellent thing to post on the internet. 10-25
Total Estimated Hours (Upper estimate includes optional steps) (inc. 10% buffer): 275-754
Esitmate / person if four people involved: (5% added) 72-198

 

The final estimate for a 4 person team assuming 3 terms at 10 weeks each comes out to be 3.4 - 7.6 hours per week per person devolted to the project. (I have included one hour for a weekly advisor meeting in the weekly esitimate). I have had to make an educated guess on some of the steps, so unforunately the estimates may be way off. I also have not included any senior design deliverables such as papers or a website, or "tutorials" as Dr. Oh likes his students to create. Depending on how these estimates shape up, this could certainly be a viable senior design project. It would be suitable for a smalle team as well (perhaps three students) as the time estimate now stands.

 

Good luck. To anyone who continues this project: please feel free to contact me regarding the 2DOF Helicopter project. I'd be happy to try to recall anything from my experience with it, and give any direction or advice I could.

 

Last Updated on Wednesday, 10 December 2008 03:56