es 100 micro aerial vehicle group 1
DESCRIPTION
ES 100 Micro Aerial Vehicle Group 1. Michelle Helsel, Austin Dickey, Alsia Plybeah , Dylan Carlson, Peter, Lucilla Calderon . Introduction. The Micro Aerial Vehicle (MAV) is a model Unmanned Aerial Vehicle (UAV) using microelectronics - PowerPoint PPT PresentationTRANSCRIPT
ES 100 Micro Aerial Vehicle
Group 1
Michelle Helsel, Austin Dickey, Alsia Plybeah, Dylan Carlson, Peter, Lucilla
Calderon
Introduction
• The Micro Aerial Vehicle (MAV) is a model Unmanned Aerial Vehicle (UAV) using
microelectronics• UAV control commands originate from remote
locations, such as a computer system, a pilot in another vehicle, or a technology team miles away
• We decided to build our MAV from scratch using our background knowledge
Objectives• We are tasked with designing and testing a micro
aerial vehicle that will:– Cost less than $250– Fly 5+ minutes without recharging its energy source – Take off from and land on the ground– Can be controlled remotely by a 2.4G Hz radio
transmitter in a 100’x50’x30’ space– And weigh less than 450 grams
• The Mission: Endurance - fly as many figure 8 paths around two pylons separated by 50’ in five minutes.
Gantt Chart through today
Gantt Chart for upcoming weeks
Bill of Materials
Design Details - Wing
• Flying wing design: chosen because it is a simple design to build from scratch as opposed to a design with a fuselage.
• Large wing area allows for lots of lift and slow flight.
• Slight dihedral and swept back wings: increases stability of the aircraft.
Design Details – Control Commands
• Flying wing type aircraft use "elevons", which act as ailerons and elevators simultaneously rather than having independent ailerons and elevators
• This design is more efficient because it combines the two
motions into one element
Design Details – Radio Commands
Design Details – Airfoil
• Asymetrical (cambered) airfoil• Airfoil name: Sipkill• Advantage: more lift at a horizontal position
than a symmetrical airfoil• Chosen because this needs to be a slow flying
aircraft for surveillance. • More lift = slower speed required for flight.
Design Details - Propeller
• Propeller: front positioning, "puller" propeller• The vehicle must take off and cannot be
thrown, so a rear propeller location would exceed the constraints
• A rear propeller would contact the ground unless unwieldy landing gear was used to elevate the wing high off the ground
Design Details - Material
• Frame constructed with balsa, covered with microlite vinyl iron-on covering
• Balsa is one of the best materials to use because of how light it is, which is important for a slow-flyer
Design Details – Landing Gear
• 3 wheels of a 3 inch diameter will be connected to the micro aerial vehicle to provide a safe and gradual landing onto the ground
Design Details - Motor
• Connects to the propeller using rubber rings, making a motor mount unnecessary
Design Details - Receiver
Design Details - Battery
In Conclusion…
We thank you for your attention to our presentation.