Trajectory optimization of a deflectable nose missile
نویسندگان
چکیده
منابع مشابه
Modeling and Simulation Research on Dynamics of Missiles with Deflectable Nose Control
The dynamic characteristics of deflectable nose missiles with rotary single-channel control were investigated in this paper. Firstly, the effective angle of attack, effective angle of sideslip and quasi-body coordinates were introduced based on the spin characteristics of the missile’s body. Secondly, considering the interaction between the missile’s nose and body, the rigid kinetic model of mi...
متن کاملBallistic missile trajectory prediction using a state transition matrix
A method for the determination of the trajectory of a ballistic missile over a rotating, spherical Earth given only the launch position and impact point has been developed. The iterative solution presented uses a state transition matrix to correct the initial conditions of the ballistic missile state vector based upon deviations from a desired set of final conditions. A six-degree-of-freedom si...
متن کاملTrajectory Optimization for a Multistage Launch Vehicle Using Nonlinear Programming
This work is an example of application of nonlinear programming to a problem of three-dimensional trajectory optimization for multistage launch vehicles for geostationary orbit missions. The main objective is to minimize fuel consumption or equivalently to maximize the payload. The launch vehicle considered here, Europa-II, consists of 5 thrust phases and 2 coast phases. Major parameters of the...
متن کاملAn Interior Trajectory Simulation of the Gas-steam Missile Ejection
An interior trajectory simulation of the canister launched missiles has been developed with the help of FLUENT. One of the special features of this simulation is the method by which the coupled three-phase problem is reduced to solving the fluid equations only. Several new source terms describing the influence of droplets and particles on gas have been created in the present case and added to t...
متن کاملRobot Arm Trajectory Planning Using Missile Guidance Algorithm
This paper presents a novel approach to on-line trajectory planning of robot arms for the interception of a fastmaneuvering object under torque and velocity constraints. Especially, the trajectory planning in the Y direction employs a missile guidance algorithm to intercept the maneuvering object. The proposed method yields that a robot arm can smoothly grasp a maneuvering object. Simulation re...
متن کاملذخیره 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: Defence Technology
سال: 2017
ISSN: 2214-9147
DOI: 10.1016/j.dt.2017.05.001