Model Predictive Static Programming Rendezvous Trajectory Generation of Unmanned Aerial Vehicles

This paper addresses the problem of threedimensional rendezvous trajectory generation for fixed-wing unmanned aerial vehicles. A time control method is developed based on the model predictive static programming which features explicit closed-form solutions and terminal output constraints. In addition to the terminal output constraints, a time-varying weighting matrix is designed in the cost function to enforce the terminal bank angle of aircraft. A two-step strategy is proposed where the first step determines feasible trajectories for every agent to pursuit a maneuvering virtual target and the second step achieves time coordination and synchronizations of position, velocity and bank angle among vehicles. Considering the nonlinear aircraft dynamics and first order input lags, numerical simulation results demonstrate the effectiveness of the proposed scheme.

[1]  Alessandro Rucco,et al.  Optimal Rendezvous Trajectory for Unmanned Aerial-Ground Vehicles , 2018, IEEE Transactions on Aerospace and Electronic Systems.

[2]  Guang Li,et al.  Optimal Cooperative Guidance Law for Salvo Attack: An MPC-Based Consensus Perspective , 2018, IEEE Transactions on Aerospace and Electronic Systems.

[3]  Fumiaki Imado,et al.  A New Missile Guidance Algorithm Against A Maneuvering Target , 1998 .

[4]  Florian Holzapfel,et al.  Optimal Rendezvous Guidance Laws with Application to Civil Autonomous Aerial Refueling , 2018 .

[5]  F. Fisch Development of a Framework for the Solution of High-Fidelity Trajectory Optimization Problems and Bilevel Optimal Control Problems , 2011 .

[6]  Anusna Chakraborty,et al.  Cooperative Simultaneous Arrival of Unmanned Vehicles onto a Moving Target in GPS-Denied Environment , 2018, 2018 IEEE Conference on Decision and Control (CDC).

[7]  Koray S. Erer,et al.  Impact Time and Angle Control Based on Constrained Optimal Solutions , 2016 .

[8]  Alessandro Rucco,et al.  Optimal UAV Rendezvous on a UGV , 2016 .

[9]  Kapil Sachan,et al.  Waypoint Constrained Multi-Phase Optimal Guidance of Spacecraft for Soft Lunar Landing , 2019, Unmanned Syst..

[10]  Rajnikant Sharma,et al.  Cooperative-timing Attack with Smart Munitions using Cooperative Localization in Contested Environments , 2016 .

[11]  Radhakant Padhi,et al.  Model Predictive Static Programming: A Computationally Efficient Technique For Suboptimal Control Design , 2009 .

[12]  Takeshi Yamasaki,et al.  Sliding mode-based pure pursuit guidance for unmanned aerial vehicle rendezvous and chase with a cooperative aircraft , 2010 .

[13]  Duane T. Davis,et al.  Development and testing of the intercept primitives for planar UAV engagement , 2017, 2017 International Conference on Unmanned Aircraft Systems (ICUAS).

[14]  Radhakant Padhi,et al.  Impact-Angle-Constrained Suboptimal Model Predictive Static Programming Guidance of Air-to-Ground Missiles , 2012 .

[15]  Austin L. Smith Proportional Navigation with Adaptive Terminal Guidance for Aircraft Rendezvous , 2007 .

[16]  Radhakant Padhi,et al.  A robust and high precision optimal explicit guidance scheme for solid motor propelled launch vehicles with thrust and drag uncertainty , 2016, Int. J. Syst. Sci..

[17]  Ashwini Ratnoo Variable Deviated Pursuit for Rendezvous Guidance , 2015 .

[18]  Min-Jea Tahk,et al.  Optimal UAV formation guidance laws with timing constraint , 2006, Int. J. Syst. Sci..

[19]  Joseph Z. Ben-Asher,et al.  Derivation of Formation-Flight Guidance Laws for Unmanned Air Vehicles , 2005 .

[20]  Qian Zhu,et al.  Time-optimal trajectory generation for aerial coverage of urban building , 2019 .