MAAV Design Requirements and Desired Features, Study Guides, Projects, Research of Electrical and Electronics Engineering

The absolute minimum requirements and desired features for the design of a micro aerial autonomous vehicle (maav). The maav must maintain stable flight, execute precise turns, have a minimum flight time, sense orientation, transmit video feed, and operate autonomously within a certain radius. Desired features include automatic gps coordination, telemetry data transmission and storage, and soft belly landing. The entire control system must not exceed 150g and use no more than 300ma.

Typology: Study Guides, Projects, Research

Pre 2010

Uploaded on 08/30/2009

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Absolute Minimum Requirements
The MAAV must be able to:
maintain straight and level flight through varying weather conditions
execute precise turns with no overshoot in varying weather conditions
have a flight time of at least 20 minutes
sense physical orientation at a frequency of at least 100hz
transmit video feed a minimum of 500 feet to a ground station
Plane must be able operate autonomously within at least a 1000ft radius of the launch
location.
“pass through” external control signals when a ground operator wishes to override the
autopilot
“seamless” conversion to autonomous control when plane is out of range of controller
Monitor battery level and take action to ensure a safe landing in case of low battery
On board electronics may not use more than 300mA average
Entire control system must not weigh more than 150g
Desired Feature Set
If possible, the MAAV may be able to:
Enable plane to fly to downloaded GPS coordinates automatically: A pass of within 30m
at any elevation shall be considered hitting the coordinate successfully.
transmit telemetry data a minimum of 500 feet to a ground station
Store telemetry data on an onboard data logger when out of contact with ground station
Continue flight to a limited extent after losing GPS data
detect when aircraft has been launched by hand and take appropriate actions to gain
airspeed and altitude
approach a predetermined landing spot from the correct direction and execute a soft belly
landing

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Absolute Minimum Requirements

The MAAV must be able to:

  • maintain straight and level flight through varying weather conditions
  • execute precise turns with no overshoot in varying weather conditions
  • have a flight time of at least 20 minutes
  • sense physical orientation at a frequency of at least 100hz
  • transmit video feed a minimum of 500 feet to a ground station
  • Plane must be able operate autonomously within at least a 1000ft radius of the launch location.
  • “pass through” external control signals when a ground operator wishes to override the autopilot
  • “seamless” conversion to autonomous control when plane is out of range of controller
  • Monitor battery level and take action to ensure a safe landing in case of low battery
  • On board electronics may not use more than 300mA average
  • Entire control system must not weigh more than 150g

Desired Feature Set

If possible, the MAAV may be able to:

  • Enable plane to fly to downloaded GPS coordinates automatically: A pass of within 30m at any elevation shall be considered hitting the coordinate successfully.
  • transmit telemetry data a minimum of 500 feet to a ground station
  • Store telemetry data on an onboard data logger when out of contact with ground station
  • Continue flight to a limited extent after losing GPS data
  • detect when aircraft has been launched by hand and take appropriate actions to gain airspeed and altitude
  • approach a predetermined landing spot from the correct direction and execute a soft belly landing