An analysis tool for collision avoidance manoeuvres using aerodynamic drag

نویسندگان

چکیده

Aerodynamic collision avoidance manoeuvres provide an opportunity for satellites in Low Earth Orbits to reduce the risk during close encounters. With rising numbers of and objects orbit, experience encounters more frequently. Especially those without thrusting capabilities face problem not being able performimpulsive evasive manoeuvres. For Orbits, though, perturbing forces due aerodynamic drag may be used influence their trajectories, thus offering a possibility avoid collisions. This work introduces tool analysis Current space-weather data are employed estimate density satellite Achievable in-track separation distances following variation ballistic coefficient through change attitude then derived by evaluating analytical equation from literature. Considering additional constraints attitude, e.g., charging phases, uncertainties parameters, manoeuvre on conjunction geometry probability is examined. The university Flying Laptop University Stuttgart as exemplary analysis, which show general effectiveness employing drag. First manoeuvring strategies can deducted parameter assessed.

برای دانلود باید عضویت طلایی داشته باشید

برای دانلود متن کامل این مقاله و بیش از 32 میلیون مقاله دیگر ابتدا ثبت نام کنید

اگر عضو سایت هستید لطفا وارد حساب کاربری خود شوید

منابع مشابه

Smart morphable surfaces for aerodynamic drag control.

Smart Morphable Surfaces enable switchable and tunable aerodynamic drag reduction of bluff bodies. Their topography, resembling the morphology of golf balls, can be custom-generated through a wrinkling instability on a curved surface. Pneumatic actuation of these patterns results in the control of the drag coefficient of spherical samples by up to a factor of two, over a range of flow conditions.

متن کامل

analysis of ruin probability for insurance companies using markov chain

در این پایان نامه نشان داده ایم که چگونه می توان مدل ریسک بیمه ای اسپیرر اندرسون را به کمک زنجیره های مارکوف تعریف کرد. سپس به کمک روش های آنالیز ماتریسی احتمال برشکستگی ، میزان مازاد در هنگام برشکستگی و میزان کسری بودجه در زمان وقوع برشکستگی را محاسبه کرده ایم. هدف ما در این پایان نامه بسیار محاسباتی و کاربردی تر از روش های است که در گذشته برای محاسبه این احتمال ارائه شده است. در ابتدا ما نشا...

15 صفحه اول

The Aerodynamic Drag of Parafoils

The parafoil is an aerodynamic decelerator that uses the concept of parachute and airfoil aerodynamics. The device has been used as a parachute for high-precision delivering of payload (military and civilian), to recover sounding rockets, for various tethered applications (to carry instrumentation for weather survey, air pollution measurements, radar tracking systems), and as recreational parac...

متن کامل

Verification of Collision Avoidance Systems Using Reachability Analysis

This paper presents a method for formal verification of automotive collision avoidance systems. Using viability theory and reachability analysis, we define when the system should intervene, i.e. the unsafe set, and when the system should not intervene, i.e. the safe set. Given these sets, we formulate the problem of verifying that a given system does not make incorrect decisions as an optimizat...

متن کامل

ذخیره در منابع من


  با ذخیره ی این منبع در منابع من، دسترسی به آن را برای استفاده های بعدی آسان تر کنید

ژورنال

عنوان ژورنال: Acta Astronautica

سال: 2023

ISSN: ['1879-2030', '0094-5765']

DOI: https://doi.org/10.1016/j.actaastro.2023.05.038