Refine
Has Fulltext
- yes (17) (remove)
Is part of the Bibliography
- yes (17)
Year of publication
Document Type
- Journal article (16)
- Conference Proceeding (1)
Language
- English (17)
Keywords
- Quadrocopter (4)
- Autonomous UAV (3)
- Quadrotor (3)
- UAV (3)
- navigation (3)
- distance measurement (2)
- unmanned aerial vehicles (2)
- Attitude Heading Reference System (AHRS) (1)
- CEF (1)
- Cooperative UAV (1)
- CubeSat (1)
- CubeSat GNSS (1)
- DNA storage (1)
- Data Fusion (1)
- DecaWave (1)
- Design and Development (1)
- Differential GPS (DGPS) (1)
- Directed Flight (1)
- Distributed Control (1)
- Flugkörper (1)
- Formation Flight (1)
- GPS (1)
- GPS Reciever (1)
- Global Navigation Satellite System (GNSS) (1)
- Global Positioning System (GPS) (1)
- Instrument Control Toolbox (1)
- MEMS IMU (1)
- Matlab (1)
- Mini Unmanned Aerial Vehicle (1)
- Mobile Sensor Network (1)
- Optical Flow (1)
- Positioning (1)
- RINEX Format (1)
- Real-time Kinematics (RTK) (1)
- Rodos (1)
- UWB (1)
- Unmanned Aerial Vehicle (1)
- Unmanned Aerial Vehicle (UAV) (1)
- Vision Based (1)
- adaptation models (1)
- aerodynamics (1)
- attitude determination (1)
- autonomous (1)
- autonomous UAV (1)
- collision avoidance (1)
- concurrent design facility (1)
- dependable software (1)
- distributed control (1)
- extended Kalman filter (1)
- force feedback (1)
- formation flight (1)
- harness free satellite (1)
- helicopters (1)
- heterogeneous background (1)
- infrared (1)
- infrared detectors (1)
- insect tracking (1)
- intelligent transportation systems (1)
- intelligent vehicles (1)
- laser ranging (1)
- light-gated proteins (1)
- magnetometer (1)
- marine navigation (1)
- mathematical model (1)
- model following (1)
- movement ecology (1)
- multirotors (1)
- nanocellulose (1)
- natural environment (1)
- obstacle detection (1)
- pose estimation (1)
- positioning (1)
- protein chip (1)
- quadcopter (1)
- quadcopters (1)
- quadrocopter (1)
- quadrotor (1)
- real-time (1)
- requirements management (1)
- robustness (1)
- rotors (1)
- satellite technology (1)
- scalable quadcopter (1)
- self-aware computing (1)
- single-electron transistors (1)
- space missions phases (1)
- structural battery (1)
- thrust vector control (1)
- ultrasonic autonomous aerial vehicles (1)
- unmanned aerial vehicle (1)
- vehicle dynamics (1)
- waypoint parameter (1)
- wireless-bus (1)
Institute
The design and implementation of a satellite mission
is divided into several different phases. Parallel to these phases an evolution of requirements will take place. Because so many people in different locations and from different background have to work in different subsystems concurrently the ideas and concepts of different subsystems and different locations will diverge. We have to bring them together again. To do this we introduce synchronization points. We bring representatives from all subsystems and all location in a Concurrent Engineering Facility (CEF) room together. Between CEF sessions the different subsystems will diverge again, but each time the
diversion will be smaller. Our subjective experience from test projects says this CEF sessions are most effective in the first phases of the development, from Requirements engineering until first coarse design. After Design and the concepts are fix, the developers are going to implementation and the concept divergences will be much smaller, therefore the CEF sessions are not a very big help any more.