The
design of the aerobots is determined by a number of constraints,
among which the weight-to-lift ratio holds the most important
place and influences all other characteristics. The lifting
force of helium at sea level, at normal conditions of pressure
and temperature, is roughly 1000g for 1 cubic meter of helium.
For instance, the large non-robotized blimp built in Moncton
in 98 (see page "Origins") is a 3,30m-edge structure,
which gives about 32 kg of lift ; the total weight of the
blimp, made of pink extruded styrofoam, was about 30 kg,
so the lifting force is 2kg, which is more than enough to
keep it flying.
The
size of the first robotized Mascarillon aerobot is 180cm
(hence the model name, M180); the lifting force is about
5300g. This may seem a lot ; the M180 is actually quite
large, and was designed as a test platorm to allow multiple
software and mechatronics tests with minimal concerns about
flying abilities. The challenge is actually to built the
smallest possible blimp : reducing the edges by a certain
factor decreases the lifting power by about the third power
of this factor, and the following models, the M170 and the
M160, see their lifting power reduced to about 4500g and
3700g respectively. Considering the fact that the load must
include the structure (about 1000g), the films (about 1500g),
the CPU, the motor controllers, the sensors, the wireless
card, the batteries, the motors and the motor ducts, the
cameras, the bonding device, and all the wires and cables,
it is easy to see that each element must be very carefully
chosen in order to maximize its general efficiency.
Apart
form theses hydrostatic considerations, many major concerns
have to be considered :
1)
- The necessity to obtain a perfect cube,
with straight edges and flat faces. This is first an art/architecture
goal, since it relates to the initial intention of creating
perfectly geometrical flying shapes, but it is also induced
by the fact that the cubes need to assemble while flying.
If the edges are not perfectly straight, or if the faces
become convex due to the internal pressure of helium, the
cubes will not assemble properly.
2)
- The self-assemblage properties. When
two cubes connect to each other, they must still be able
to use their motors to move in space. The air stream output
by the motors of the two cubes must add in order to maintain
an adequate thrust. This led to the decision to place the
ducted fans at the midpoint of each edge, and to guide the
air streams with thin plastic or paper tubes to the corners
of the cube.
3)
- The axial symmetry of the cubes. The
cube is oriented in space : it has a top and a bottom. All
equipments is located within the bottom edges and corners,
except for the four z-axis ducted fans, which are placed
at the middle of the vertical trusses. In order to preserve
horizontal stability and to symmetrize the angular momentum
of the whole cube, all elements are located within the center
section of the trusses and/or at the corners of the cube.
Each element must be counterweighted by another element
located in the opposite corner or truss center. No helix
configuration is allowed : no element can be located off
the corners or off the middle section of the trusses, since
his would introduce asymmetries in the angular momentum.
4)
- The location of the sensors. This is
a critical concern. The cube is by no way an optimal shape
when it comes to sensory aptitudes, especially with large
cubes such as the M180. Obstacle avoidance would ideally
require 24 sensors (one for each axis on each edge), which
is hard to implement for reasons of cost and energy requirements.
The optimal location is still being studied ; three 14-sensors
Mascarillons are flying since August 2005.
5)
- The need for assembling and disassembling the
cubes. Transportation of the cubes is a major concern
: these big, hollow shapes would be very costly to move
for a demo or an experiment, and since the trusses are also
quite fragile, the structure must designed in order to allow
the disassembling of the cubes, and their storage in small
protecting cases.