In theory, with active stabilization DARE would be able to safely launch rockets into space. Flight control related faults can have severe impact on crew and ve- hicle safety during ascent. With this new technology, DARE is able to extends its current rocket designs to even higher levels. INTRODUCTION This paper is focused on the developement of algorithms for vehicle health management (VHM) of a launch vehicle in closed-loop ight including vehicle dynamics, ight control actuators, sensors, navigation, and propulsion system. The launch of the V7S was a turning point of the whole DARE society. Furthermore, the team is investigating a new type of stabilization system which does not have this problem, such as fin-stabilization.
![rocket flight control system rocket flight control system](http://www.howitworksdaily.com/wp-content/uploads/2015/12/Soyuz-launch-system-1024x643.jpg)
To solve this problem, future rocket configurations which use canards should not have the canards in-line with the fins. Unfortunately the team does not have the tools or knowledge to study this aerodynamic interference effect in detail, since it most likely requires 3D Computational Fluid Dynamics vorticity analysis, which is a very specialized field in aerodynamics. This is probably caused by an aerodynamic interference effect between the canards and fins during a roll-stabilized flight. This was accomplished by first creating a simulation of the rockets flight path using a six degree-of-freedom mathematical model. The flight tests in May and September concluded that the overall stabilization system worked, however that the canards in the current configuration are not optimal.
#Rocket flight control system software
To reduce the risk during flight, the rocket was limited via software to only perform roll stabilization.
![rocket flight control system rocket flight control system](https://www.yugoimport.com/sites/default/files/slika-2_4.gif)
The objective of the first flight test was to perform a complete integrated flight test of the sensors, flight computer, control algorithms, and canards. After an unfortunate attempt in Denmark in April, the first flight of the V7S took place in May.
![rocket flight control system rocket flight control system](https://www.yugoimport.com/sites/default/files/t-7_0.jpg)
In 2016 the ACT performed the first flights with the actively stabilized V7S rocket. the efficiency of rocket propulsion of spacecraft is considered in terms of the control of propellant consumption, trajectory planning, and in-flight.