Results 41 to 50 of about 75,283 (193)
Finite-Time Distributed Cooperative Guidance Law with Impact Angle Constraint
International Journal of Aerospace Engineering, 2023 The problem of the distributed cooperative guidance law of multiple missiles attacking a stationary target with impact angle constraint is investigated.
Wenguang Zhang, Jin Yan
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Analytical control laws for interplanetary solar sail trajectories with constraints [PDF]
, 2008 An indirect method is used to obtain an analytical control law for a spacecraft with a low-thrust propulsion system which is constituted by a solar sail coupled with a solar electric thruster. Constraints on the control inputs for such as the system need
McInnes, C.R., Uchiyama, Kenji
core
Three-Dimensional Impact Time and Angle Control Guidance Based on MPSP
International Journal of Aerospace Engineering, 2019 A new nonlinear guidance law for air-to-ground missile cooperation attacks is proposed in this paper. This guidance law enables missiles with different initial conditions to attack targets simultaneously, and it can also precisely satisfy the terminal ...
Yang Li, Hao Zhou, Wanchun Chen
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IEEE Access, 2019 In this paper, considering a class of skid-to-turn (STT) missile with impact angle constraint to intercept the maneuvering target, a three-dimensional integrated guidance and control law based on the fractional integral terminal sliding mode control ...
Xinghe Zhou +4 more
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Optimal Cooperative Guidance Laws for Two UAVs Under Sensor Information Deficiency Constraints
Sensors, 2020 This paper presents closed-form optimal cooperative guidance laws for two UAVs under information constraints that achieve the required relative approach angle.
Daniel Lee, Han-Lim Choi, Jong-Han Kim
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Mathematics, 2023 This paper proposes a CKF-MPSP guidance method for hitting stationary targets with impact time and angle constraints for missiles in the presence of modeling errors.
Zihan Xie +3 more
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A Practical Optimal Guidance Scheme Under Impact Angle and Terminal Acceleration Constraints
International Journal of Aeronautical and Space Sciences, 2021 This paper proposes a practical optimal guidance law that can handle terminal angle and acceleration constraints while providing robustness against uncertainty in autopilot dynamics. Building upon a well-established linear-quadratic optimal guidance framework, we first derive an energy-minimizing guidance scheme that nullifies terminal acceleration ...
Hyo-Seon Chi +3 more
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Вестник Самарского университета: Аэрокосмическая техника, технологии и машиностроение, 2020 The paper deals with disturbed motion of the hypersonic first stage of an aerospace system in accelerated climb. Disturbances are deviations of atmospheric density from the values of a standard model. A multistep control process is accepted.
M. M. Krikunov
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DronesThis paper addresses the guidance of various flight vehicles under multiple constraints in three-dimensional space. A cooperative guidance strategy that satisfies both time and angle constraints is designed to reach a moving target.
Ao Li +3 more
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A Novel Guidance Law for Intercepting a Highly Maneuvering Target
International Journal of Aerospace Engineering, 2021 Given the resolution of the guidance for intercepting highly maneuvering targets, a novel finite-time convergent guidance law is proposed, which takes the following conditions into consideration, including the impact angle constraint, the guidance ...
Gang Wu, Ke Zhang
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